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SITRO-AIS-27

In orbit NORAD 59068 TFHP-8381-2856-3771-0898

Soyuz 2.1b Fregat-M

Carrier rocket

Cosmodrome Site 1S

Spaceport

280

Observations all time

Mission information
Spacecraft name
SITRO-AIS-27
Other names
SC2315
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Soyuz 2.1b Fregat-M
Upper stage
Фрегат-М
Spaceport
Cosmodrome Site 1S
Launch time
2024-02-29 05:43:26
Separation time
Last observers
Observer
Time of receipt
2026-08-18 18:57:53 UTC
2026-08-18 17:20:01 UTC
2026-08-17 20:26:27 UTC
2026-08-04 06:25:14 UTC
2026-08-03 17:14:24 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
483.57 km
Apogee
678.81 km
Inclination
95.4°
Period
96.4 min
Semi-major axis
6959.3 km
Velocity
7.46 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 06:09:03 UTC
Two-line elements (TLE)
1 59068U 24039T   26285.95644970  .00003802  00000-0  29325-3 0  9990
2 59068 95.3771 316.1683 0140239 275.0184 83.5047 14.94394303142325
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-14 06:49:34 STARLINK-4440
NORAD 53671
SITRO-AIS 27
NORAD 59068
1.927 14.86 1.4e-05
2026-10-14 07:52:50 SITRO-AIS 27
NORAD 59068
SCOUT X-4 R/B
NORAD 1815
1.856 15.07 5.9e-07
2026-10-14 08:20:43 COSMOS 2567
NORAD 55978
SITRO-AIS 27
NORAD 59068
4.065 11.88 1.8e-07
2026-10-14 11:00:50 SITRO-AIS 27
NORAD 59068
KUIPER-00646
NORAD 69789
4.476 14.30 9.9e-08
2026-10-15 02:51:00 SITRO-AIS 27
NORAD 59068
NOAA 16 DEB
NORAD 41227
4.928 12.92 1.1e-07
2026-10-15 06:47:00 SITRO-AIS 27
NORAD 59068
OBJECT AE
NORAD 67276
2.823 5.58 5.2e-07
2026-10-17 23:23:39 SITRO-AIS 27
NORAD 59068
STARLINK-36055
NORAD 66846
0.417 15.01 2.7e-04
2026-10-18 04:12:21 SITRO-AIS 27
NORAD 59068
STARLINK-35982
NORAD 66828
1.969 15.01 1.2e-05
2026-10-18 05:48:38 SITRO-AIS 27
NORAD 59068
STARLINK-35982
NORAD 66828
4.750 15.01 2.1e-06
2026-10-18 22:22:03 SITRO-AIS 27
NORAD 59068
FENGYUN 1C DEB
NORAD 37424
3.168 6.03 4.1e-07
2026-10-19 04:02:04 SITRO-AIS 27
NORAD 59068
OBJECT P
NORAD 64889
4.414 7.62 2.0e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite