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SITRO-AIS-40

In orbit NORAD 61776 NRCG-0362-0567-0567-5483 Спутникс

Time in UTC

13.10 06:55

Scheduled · JHR

39

Observations over 30 days

83%

Successful observations

4k

Frames, latest 2026-10-11 20:16 UTC

Mission information
Spacecraft name
SITRO-AIS-40
Other names
SC2328
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 20:16:47 UTC
2026-10-11 06:18:40 UTC
2026-10-10 19:55:19 UTC
2026-10-08 22:11:35 UTC
2026-10-08 20:43:02 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
329.96 km
Apogee
335.91 km
Inclination
97.3°
Period
91.2 min
Semi-major axis
6710.2 km
Velocity
7.71 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 06:09:04 UTC
Two-line elements (TLE)
1 61776U 24199AT  26285.89864747  .00146064  00000-0  83892-3 0  9992
2 61776 97.2614 166.8764 0004650 153.2516 206.8991 15.78335814156073
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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 14:54:56 STARLINK-30776
NORAD 58136
SITRO-AIS 40
NORAD 61776
1.282 13.82 4.4e-05
2026-10-14 05:37:49 JILIN-1 GAOFEN 3F
NORAD 46458
SITRO-AIS 40
NORAD 61776
3.921 15.26 1.0e-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