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SATURN

In orbit NORAD 57174 KATA-8177-7690-1660-7290 Russia

Time in UTC

07:00

Next pass · Чукотка · 56°

—

No observations scheduled

3

Observations over 30 days

86%

Successful observations

591

Frames, latest 2026-10-03 20:03 UTC

Mission information
Spacecraft name
SATURN
Other names
САТУРН, RS43S
Call sign
RS43S
Frequency usage status
Violator
Network
УниверСат
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
2023-06-27 11:34:00
Separation time
Last observers
Observer
Time of receipt
2026-09-14 17:49:59 UTC
2026-06-12 20:04:09 UTC
2025-09-02 20:08:50 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
509.17 km
Apogee
529.35 km
Inclination
97.5°
Period
95.1 min
Semi-major axis
6897.4 km
Velocity
7.58 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:34 UTC
Two-line elements (TLE)
1 57174U 23091J   26284.95229583  .00004907  00000-0  26885-3 0  9996
2 57174 97.4917 336.3485 0014664 103.3413 256.9455 15.14578712181301
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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 18:16:51 Z-SAT
NORAD 49399
OBJECT J
NORAD 57174
2.855 2.57 5.3e-07
2026-10-13 09:21:51 CUTE-1.7+APD II (CO-65)
NORAD 32785
OBJECT J
NORAD 57174
4.930 8.32 1.6e-07
2026-10-13 18:40:26 STARLINK-3739
NORAD 52266
OBJECT J
NORAD 57174
2.377 13.52 1.3e-05
2026-10-14 00:47:04 AAC-HSI-SAT1
NORAD 56225
OBJECT J
NORAD 57174
4.700 15.08 7.1e-08
2026-10-14 20:53:49 OBJECT J
NORAD 57174
THORAD AGENA D DEB
NORAD 4157
1.746 14.68 6.0e-07
2026-10-15 05:38:54 STARLINK-5286
NORAD 55294
OBJECT J
NORAD 57174
2.660 13.73 9.8e-06
2026-10-15 08:55:08 OBJECT J
NORAD 57174
COSMOS 1275 DEB
NORAD 15767
4.740 14.08 9.5e-08
2026-10-15 09:41:45 OBJECT J
NORAD 57174
AC1-003
NORAD 66689
3.116 2.57 4.5e-07
2026-10-16 00:42:29 OBJECT J
NORAD 57174
OBJECT E
NORAD 62733
4.653 12.90 1.2e-07
2026-10-16 01:44:22 STARLINK-5048
NORAD 53911
OBJECT J
NORAD 57174
3.799 9.15 7.6e-06

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