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SATURN

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

Time in UTC

07:24

Next pass · Обозерский

—

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
509.18 km
Apogee
529.35 km
Inclination
97.5°
Period
95.1 min
Semi-major axis
6897.4 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:37 UTC
Two-line elements (TLE)
1 57174U 23091J   26283.89522175  .00005258  00000-0  28789-3 0  9996
2 57174 97.4920 335.3076 0014620 106.6089 253.6749 15.14568875181148
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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 02:47:42 STARLINK-4620
NORAD 53674
OBJECT J
NORAD 57174
3.879 15.08 3.1e-06
2026-10-12 04:22:47 STARLINK-4620
NORAD 53674
OBJECT J
NORAD 57174
3.709 15.08 3.4e-06
2026-10-12 18:16:52 Z-SAT
NORAD 49399
OBJECT J
NORAD 57174
4.667 2.57 2.0e-07
2026-10-13 05:43:48 OBJECT J
NORAD 57174
SHIJIAN-30A (SJ-30A)
NORAD 66545
3.369 5.99 3.6e-07
2026-10-14 00:47:06 AAC-HSI-SAT1
NORAD 56225
OBJECT J
NORAD 57174
4.586 15.08 7.4e-08
2026-10-15 03:23:39 OBJECT J
NORAD 57174
NUSAT-54 (BRANCA MARQUES)
NORAD 68442
4.882 11.09 1.3e-07
2026-10-15 12:57:15 STARLINK-5917
NORAD 55942
OBJECT J
NORAD 57174
0.669 12.49 1.9e-04
2026-10-16 00:42:32 OBJECT J
NORAD 57174
OBJECT E
NORAD 62733
4.742 12.90 1.2e-07
2026-10-16 07:07:35 XINGYUN-2 01
NORAD 45602
OBJECT J
NORAD 57174
1.367 7.65 2.1e-06
2026-10-16 07:12:50 STARLINK-5539
NORAD 55747
OBJECT J
NORAD 57174
3.135 8.80 1.1e-05

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