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Sirius-SINP-3U

In orbit NORAD 57185 BFNY-6054-1647-2729-6927 Russia

Soyuz 2.1b Fregat-M

Carrier rocket

Cosmodrome Site 1S

Spaceport

2

Observations all time

Mission information
Spacecraft name
Sirius-SINP-3U
Other names
R6DRF
Call sign
-
Frequency usage status
Violator
Network
Space-п
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
2023-06-27 11:34:00
Separation time
Last observers
Observer
Time of receipt
2024-12-23 08:53:36 UTC
2024-12-23 07:21:02 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
428.02 km
Apogee
436.15 km
Inclination
97.5°
Period
93.3 min
Semi-major axis
6810.2 km
Velocity
7.64 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:56 UTC
Two-line elements (TLE)
1 57185U 23091V   26283.58210050  .00025428  00000-0  56350-3 0  9996
2 57185 97.4946 357.4463 0005921 31.3653 328.7947 15.43733849182555
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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 22:28:11 OBJECT V
NORAD 57185
TRANSPORTER-6 OBJECT H
NORAD 55016
1.640 1.24 1.6e-06
2026-10-13 23:14:49 OBJECT V
NORAD 57185
TRANSPORTER-6 OBJECT H
NORAD 55016
3.611 1.24 3.4e-07
2026-10-13 23:34:12 OBJECT V
NORAD 57185
NUSHSAT1
NORAD 63211
4.440 15.16 8.0e-08
2026-10-15 07:21:56 STARLINK-2514
NORAD 48331
OBJECT V
NORAD 57185
3.996 14.40 3.8e-06
2026-10-15 18:13:08 OBJECT V
NORAD 57185
SPACEMOBILE-004 DEB
NORAD 62372
4.388 8.61 1.9e-07
2026-10-16 01:13:12 OBJECT V
NORAD 57185
SPACEMOBILE-004 DEB
NORAD 62372
4.253 8.50 2.1e-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