Showing posts with label upper stage. Show all posts
Showing posts with label upper stage. Show all posts

Monday, 9 June 2025

The reentry of the Chinese Zhuque-2E upper stage 2025-103G over Kazachstan on 5 June 2025

still from one of the fireball movies posted on Twitter by @Buggy__Bugler

 

In the evening of 5 June 2025 around 22h local time (17h UTC), a slow profusely fragmenting fireball was seen and filmed from several cities in Kazachstan, including Astana, and Bishkek in neighbouring Kirgistan. It had all the well-known characteristics of a satellite or rocket stage reentry. Indeed, as it turns out, this was a rocket stage reentry: the reentry of the upper stage of a Chinese Zhuque-2E (ZQ-2E) rocket, 2025-103G, from a multiple satellite launch on May 17.

Unfortunately, some Russian and Ukranian language twitter accounts started to disseminate the footage with the wildly wrong suggestion that this was a failing Russian Oreshnik IRBM breaking up. This misinformation next proliferated very quickly via various social media, and later also traditional media (e.g. Newsweek). This while it is not a Russian Oreshnik missile at all, as already mentioned.

I was alerted to the event somewhat later that evening when several of my social media followers tagged me and asked me for my opinion. It didn't take me long to identify the event as a space-launch related reentry rather than a Russian missile. Indeed, the Kazachstan MoD had meanwhile also deemed it a space debris reentry, per various news outlets.

The object in question was 2025-103G (cat. nr. 64054), the Zhuque-2E (ZQ-2E) upper stage from a Chinese satellite launch on 17 May 2025 from Dongfeng (Jiuquan). The upper stage from this launch was left in an in initially 600 x 175 km, 96.1 degree inclined orbit.

The CsPOC TIP for this object's reentry available at that time (it was updated later), had forecast reentry at 5 June 2025, 15:40 UTC with an uncertainty of  ± 3 hours. The Kazachstan event (~17h UTC) hence was within the reentry window. When I checked the trajectory over this full window, it showed that the object would make a south-to-north pass over eastern Kazachstan around 17:10 UTC, very close in time to the Kazachstan event (which was reportedly around 10 pm local Astana time = around 17 hr UTC). Direction of movement in the various videos of the event matched well.

Later, CSpOC published a final TIP placing the reentry at 5 June 2025 17:08 UTC  ± 1 min, near 36.6 N, 73.5 E. Given the 1 minute accuracy, this is likely based on a DoD satellite observation of the reentry fireball. The TIP position is just south of Kazachstan, but a reentry is a process of several minutes duration. Moving south-to-north, the fireball created by the fragmenting space debris would move northwards, over eastern Kazachstan, in the minutes directly after this time mark. In other words, this final TIP matches the event quite well.

Below is the trajectory over the final revolution of the ZQ-2E upper stage, based on the last available TLE (epoch 25156.48638369) which dates from ~5 hours before the reentry:

 

Click map to enlarge

I next ran a reentry model with our Delft Technical University open source Astrodynamics package Tudat. The ZQ-2E upper stage has a dry mass of approximately 5000 kg and measures 12 x 3.4 meter. Using 60% of the maximum drag area for that dimension, a value usually representing the average drag surface of a tumbling (and hence showing a variable drag surface) elongated rocket stage well, the Tudat model predicts reentry near 17:03 UTC ± 1.1 hr (remember, this is based on a 5 hour old orbit), the nominal value being well in line with the Kazachstan event and nominally within 5 minutes of the CSpOC final TIP.

Next I ran the model again adjusting the drag area slightly, via trial-and-error, such that the model would conform to the estimated start of visibility of the reentry fireball, at just below  ~100 km altitude, at the time/location of the CSpOC TIP (17:08 UTC). 

I get a reasonable match when I reduce the drag area to about 58% of the maximum drag area. Below is a map showing the resulting estimated reentry trajectory (movement is from south to north):

click map to enlarge

When I use this Tudat-estimated reentry trajectory to generate a sky track for Astana, Kazachstan, I get this approximate sky trajectory (movement is from left to right, i.e. south to north, low through the west):

Click map to enlarge

This conforms quite well to some of the video footage of the reentry (several of which show the reentry fireball pass the waxing moon), e.g.:

 

still from one of the movies posted on Twitter by @Buggy__Bugler

The predicted sky track for Astana of course depends on how accurate our Tudat-modelled atmospheric altitudes of the reentering rocket stage are. If they in reality are a bit lower than we modelled, the trajectory will be located slightly lower in the sky (and vice versa, slightly higher if the altitudes are in reality a bit higher). It is very clear however that the general direction and location of the trajectory in the sky matches well with what was seen and filmed.

As usual, I feel some frustration about the general absence of information on camera locations and time of the footage regarding the imagery of this event distributed via various social networks. Those data are important but almost never included. These matches of observations with reentry data would get so much easier if people posting footage would include the geographic location and the time. So please people: next time you post something like this, include these important data.

This event once again also showed the failure of AI as a reliable source of information for answering questions regarding events like this (we earlier saw that with the Kosmos 482 Descent Craft reentry too). Twitter's AI "Grok" generated some profound nonsense (i.e., misinformation) when people asked it to identify the character of the event, likely partly as a result of the large amount of disinformation already doing the rounds on social media about this event.

Wednesday, 19 February 2025

The reentry of a Falcon 9 upper stage over NW Europe on 19 February [UPDATED]


In the early morning of February 19, 2025, near 3:45 UTC (4:45 CET) scores of people in the Netherlands, UK, Germany and Denmark saw a slow, fragmenting object move through the sky. The event garnered much attention. 

Above is a video of the event obtained by the camera of @dutchspace.bsky.social in the Netherlands.  Another stunning video, by the meteor camera of AndrĂ© Knoeffel in Brandenburg, Germany, is here. The video below is by Nick James from the UK, and shows the start of the reentry near 03:43 UTC and start of fragmentation.


The event was caused by the reentry of a SpaceX Falcon 9 upper stage, object 2025-022Y (cat nr 62878) . This upper stage, from the Starlink group 11-4 launch from Vandenberg, California, on 1 February 2025 23:02 UTC, 18 days prior to the reentry event, failed to deorbit in a controlled way after launch and payload insertion. It was supposed to do a deorbit burn after releasing the payloads, and deorbit over a specified area in the Pacific Ocean around 00:45 UTC on Feb 2, near the end of the first revolution (see map below). With the deorbit failed, it however stayed on orbit for almost 3 weeks, and then had an uncontrolled deorbit over NW Europe on February 19.

 

click map to enlarge

The general character of the Feb 19 event (slow, fragmenting) as well as time and location fit well with the Falcon 9 upper stage reentry. The CSpOC final TIP for this reentry (which we suspect is based on a satellite observation of the reentry fireball) is 19 February 3:43 UTC ± 1 min, near 52.8 N, 5.6 W. The reentry trajectory runs over the British Isles, the northern Netherlands, northern Germany and Poland.

Below is the ground-track for the last orbit up to reentry, and a detail of the approximate final reentry track over Europe, with the Netherlands indicated in red:

click map to enlarge

 
click map to enlarge

A possible piece of debris has been found at Komorniki near Poznan in Poland, media reports. The object on the photograph looks like a Composite Overwrap Pressure Vessel, a component of the Falcon 9 upper stage that has survived reentry before, e.g. in March 2021 when a Falcon 9 upper stage reentered over Washington. The location of the find matches well with the reentry trajectory, as can be seen in the map above. [update: reportedly another one of these composite-wrapped pressure tanks was subsequently found in Poland]

The event caused a lot of media attention: I did several media interviews on the reentry, amongst others with two Dutch national tv channels.


 

Sunday, 25 March 2018

The atmospheric reentry of the Soyuz upper stage 2018-026B on March 25

click map to enlarge

On March 21 at 17:44 GMT,  a Soyuz rocket (Soyuz MS-08) was launched from Baikonur in Kazakhstan, bringing three new astronauts to the International Space Station.

The upper stage from this rocket (2018-026B) reentered the atmosphere last night, producing a nice spectacle in the sky. The reentry was seen from southern Europe, and filmed from Italy. The still below is from video footage that you can find here on the Italian Ondanews website.

click image to enlarge. Link to newsitem with video

The US Military tracking network JSpOC gives a final TIP bulletin placing reentry at 25 March 1:25 UT ± 1 minute near 41.9 N, 8.1 E, depicted as a star symbol in the map in top of this page. The ± 1 minute indicates that this time and position come from an Infrared observation by one of the US Early warning satellites and hence should be very accurate.

I had been issuing forecast on twitter prior to this reentry, based on modelling in SatAna/SateEvo and GMAT. In addition to the JSpOC TIP position and time, the map above also gives some of my own modelling results for this reentry. The open circles were my two last proper forecasts, made before the actual reentry happened. The red dots are two "post-casts", i.e. forecasts made after-the -fact using orbital elements that were not yet available when I made my last forecast the evening before. The nominal position of the SatAna/SatEvo post-cast is only 10 minutes from the JSpOC TIP.