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CSTP-2.1

In orbit NORAD 61777 JYUW-3071-2314-1825-5576 Russia

Soyuz 2.1b Fregat-M

Carrier rocket

Cosmodrome Site 1S

Spaceport

53

Observations all time

Mission information
Spacecraft name
CSTP-2.1
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
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
2025-02-09 03:23:07 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
406.65 km
Apogee
423.62 km
Inclination
97.3°
Period
92.9 min
Semi-major axis
6793.1 km
Velocity
7.64 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 13:08:40 UTC
Two-line elements (TLE)
1 61777U 24199AU  26285.28215431  .00017018  00000-0  30907-3 0  9991
2 61777 97.2763 158.6992 0012585 198.7698 161.3092 15.49545229152290
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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 07:16:56 CONNECTA IOT-4
NORAD 60524
OBJECT AU
NORAD 61777
3.712 14.55 1.4e-07
2026-10-14 20:59:37 OBJECT AU
NORAD 61777
SPACEMOBILE-002 DEB
NORAD 62370
3.721 12.42 2.1e-07
2026-10-15 23:19:48 OBJECT AU
NORAD 61777
COSMOS 1461
NORAD 14064
3.576 14.79 1.4e-05
2026-10-16 03:27:55 DEIMOS
NORAD 60526
OBJECT AU
NORAD 61777
1.473 14.47 9.2e-07
2026-10-17 03:38:57 GLOBAL-13
NORAD 49773
OBJECT AU
NORAD 61777
1.081 6.71 3.4e-06
2026-10-17 08:43:15 SKYSAT-C12
NORAD 43797
OBJECT AU
NORAD 61777
3.061 14.48 1.2e-07
2026-10-17 13:20:07 CINEMA
NORAD 38764
OBJECT AU
NORAD 61777
4.476 14.20 1.1e-07
2026-10-17 20:17:28 OBJECT AU
NORAD 61777
OBJECT B
NORAD 47700
4.812 14.94 7.5e-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