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Norby-2

In orbit NORAD 57179 WSRI-6167-9286-6885-9902 Russia

Союз-2.1б

Carrier rocket

Восточный

Spaceport

3

Observations all time

Mission information
Spacecraft name
Norby-2
Call sign
-
Frequency usage status
Violator
Network
УниверСат
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
Союз-2.1б
Upper stage
Фрегат-М
Spaceport
Восточный
Launch time
2023-06-27 11:34:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
500.09 km
Apogee
522.41 km
Inclination
97.5°
Period
94.9 min
Semi-major axis
6889.4 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:48 UTC
Two-line elements (TLE)
1 57179U 23091P   26283.26459217  .00003134  00000-0  16060-3 0  9998
2 57179 97.4962 338.0911 0016193 86.9405 273.3681 15.17210047181238
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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
2026-10-11 00:59:35 OBJECT P
NORAD 57179
PIESAT-2 12
NORAD 62336
4.703 12.20 1.3e-07
2026-10-11 12:47:14 OBJECT P
NORAD 57179
OBJECT F
NORAD 63296
2.898 10.32 4.0e-07
2026-10-11 19:55:57 OBJECT P
NORAD 57179
OBJECT C
NORAD 65940
3.502 3.38 3.5e-07
2026-10-11 21:30:55 OBJECT P
NORAD 57179
OBJECT C
NORAD 65940
1.839 3.38 1.3e-06
2026-10-11 22:18:24 OBJECT P
NORAD 57179
OBJECT C
NORAD 65940
3.659 3.40 3.2e-07
2026-10-11 23:05:53 OBJECT P
NORAD 57179
OBJECT C
NORAD 65940
4.938 3.38 1.8e-07
2026-10-11 23:53:22 OBJECT P
NORAD 57179
OBJECT C
NORAD 65940
0.874 3.40 5.7e-06
2026-10-12 01:28:20 OBJECT P
NORAD 57179
OBJECT C
NORAD 65940
4.275 3.40 2.4e-07
2026-10-12 11:07:58 OBJECT P
NORAD 57179
HYDRA-3
NORAD 69022
3.629 14.85 1.3e-07
2026-10-12 13:53:02 OBJECT P
NORAD 57179
YAOGAN-39 02B
NORAD 57889
2.740 12.99 3.5e-07
2026-10-13 02:00:35 OBJECT P
NORAD 57179
OBJECT F
NORAD 68203
4.713 2.41 2.0e-07
2026-10-13 12:20:28 OBJECT P
NORAD 57179
COSMO
NORAD 68460
3.733 11.40 2.2e-07
2026-10-14 21:26:20 OBJECT P
NORAD 57179
SL-16 DEB
NORAD 29094
1.306 14.66 1.1e-06
2026-10-16 05:12:37 SHIJIAN-6 04A (SJ-6 04A)
NORAD 37179
OBJECT P
NORAD 57179
2.459 3.57 7.1e-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