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SITRO-AIS-28

In orbit NORAD 59071 QBAD-3953-1599-8847-5828

Time in UTC

06:40

Next pass · Обозерский

—

No observations scheduled

1

Observations over 30 days

43%

Successful observations

9k

Frames, latest 2026-10-09 04:55 UTC

Mission information
Spacecraft name
SITRO-AIS-28
Other names
SC2316
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
2026-10-09 04:55:36 UTC
2026-07-16 06:53:31 UTC
2026-03-11 09:14:30 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
483.62 km
Apogee
678.57 km
Inclination
95.4°
Period
96.4 min
Semi-major axis
6959.2 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:35 UTC
Two-line elements (TLE)
1 59071U 24039U   26284.92680951  .00003321  00000-0  25643-3 0  9994
2 59071 95.3778 315.5159 0140087 278.5290 80.0083 14.94425072142177
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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
2026-10-12 20:53:10 SITRO-AIS 28
NORAD 59071
COSMOS 2251 DEB
NORAD 35611
4.611 3.30 2.0e-07
2026-10-12 23:03:56 SITRO-AIS 28
NORAD 59071
KUIPER-00616
NORAD 69775
0.657 14.33 4.5e-06
2026-10-14 23:02:33 SITRO-AIS 28
NORAD 59071
SL-8 R/B
NORAD 4139
4.868 10.24 7.0e-07
2026-10-15 10:59:49 SITRO-AIS 28
NORAD 59071
MULE 4T
NORAD 67286
3.564 5.68 3.3e-07
2026-10-15 20:49:56 SITRO-AIS 28
NORAD 59071
RASSVET-3 19
NORAD 100085
4.900 15.22 6.2e-08
2026-10-16 00:02:01 SITRO-AIS 28
NORAD 59071
RASSVET-3 25
NORAD 100091
4.085 15.22 8.9e-08
2026-10-16 03:14:12 SITRO-AIS 28
NORAD 59071
RASSVET-3 27
NORAD 100093
3.916 15.22 9.6e-08
2026-10-16 04:46:58 STARLINK-5613
NORAD 55752
SITRO-AIS 28
NORAD 59071
4.094 10.82 5.9e-06
2026-10-16 23:57:24 SITRO-AIS 28
NORAD 59071
SITRO-AIS-65
NORAD 67266
4.272 5.70 2.3e-07
2026-10-17 17:58:19 SITRO-AIS 28
NORAD 59071
STARLINK-35858
NORAD 66833
2.687 15.01 6.6e-06
2026-10-18 04:58:41 SITRO-AIS 28
NORAD 59071
HERMES-1
NORAD 63242
4.697 14.20 9.6e-08

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