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SIT-HSE

In orbit NORAD 61763 PGYI-7132-9309-6598-0525 Спутникс Russia

Time in UTC

12:55

Next pass · МАН РС(Я) ГЕОСКАН УКВ · 27°

—

No observations scheduled

26

Observations over 30 days

35%

Successful observations

4k

Frames, latest 2026-10-11 06:38 UTC

Mission information
Spacecraft name
SIT-HSE
Network
Space-п
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
2024-11-04 23:18:40
Separation time
Last observers
Observer
Time of receipt
2026-10-11 06:38:07 UTC
2026-10-10 23:06:10 UTC
2026-10-10 09:03:20 UTC
2026-10-10 07:33:15 UTC
2026-10-09 06:53:16 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
378.56 km
Apogee
383.24 km
Inclination
97.3°
Period
92.2 min
Semi-major axis
6759.0 km
Velocity
7.66 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:38 UTC
Two-line elements (TLE)
1 61763U 24199AE  26283.94264702  .00092901  00000-0  10864-2 0  9995
2 61763 97.2742 162.6522 0003465 166.8907 193.2442 15.61267092155594
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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
2026-10-13 08:33:51 SIT-HSE
NORAD 61763
SL-12 R/B(AUX MOTOR)
NORAD 37143
2.515 15.08 3.5e-07
2026-10-13 16:27:10 SPACEVAN-001
NORAD 58295
SIT-HSE
NORAD 61763
4.032 14.13 1.3e-07
2026-10-13 17:13:17 SPACEVAN-001
NORAD 58295
SIT-HSE
NORAD 61763
3.995 14.17 1.4e-07
2026-10-15 22:23:29 SIT-HSE
NORAD 61763
COSMOS 2098
NORAD 20774
3.228 15.61 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