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NasbSat-2

In orbit NORAD 67285 ENMR-1106-8768-2633-2018 Спутникс Belarus

Time in UTC

04:46

Next pass · МАН РС(Я) ГЕОСКАН УКВ · 13°

—

No observations scheduled

2

Observations over 30 days

73%

Successful observations

2k

Frames, latest 2026-09-22 08:25 UTC

Mission information
Spacecraft name
NasbSat-2
Other names
A2S5A, A2S5B
Call sign
A2S5A
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
2025-12-28 13:18:05
Separation time
Last observers
Observer
Time of receipt
2026-09-22 08:25:03 UTC
2026-09-17 08:41:20 UTC
2026-09-09 08:32:12 UTC
2026-09-06 08:05:01 UTC
2026-09-05 19:09:23 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
481.97 km
Apogee
493.88 km
Inclination
97.4°
Period
94.4 min
Semi-major axis
6866.0 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 22:09:14 UTC
Two-line elements (TLE)
1 67285U 25313AP  26286.45854770  .00005656  00000-0  22962-3 0  9992
2 67285 97.3817 359.5962 0008613 309.2512 50.7961 15.24955549 43985
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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
2026-10-14 12:56:35 NASBSAT-2
NORAD 67285
BRO-21
NORAD 69007
3.535 15.10 1.3e-07
2026-10-15 20:06:54 HAWK-12A
NORAD 64623
NASBSAT-2
NORAD 67285
4.114 8.90 2.2e-07
2026-10-16 05:32:53 FLOCK 4H-33
NORAD 66736
NASBSAT-2
NORAD 67285
4.707 0.13 2.0e-07
2026-10-17 04:10:55 MALLIGYONG-1
NORAD 58400
NASBSAT-2
NORAD 67285
2.996 14.97 1.8e-07
2026-10-17 10:29:58 NASBSAT-2
NORAD 67285
CZ-4C R/B
NORAD 49123
3.223 14.90 1.7e-07
2026-10-17 15:23:21 JILIN-1 10
NORAD 43946
NASBSAT-2
NORAD 67285
1.765 3.37 1.4e-06
2026-10-17 23:53:41 STARLINK-5293
NORAD 55295
NASBSAT-2
NORAD 67285
4.315 14.96 2.7e-06
2026-10-18 08:19:45 YAOGAN-36 05A
NORAD 57452
NASBSAT-2
NORAD 67285
3.082 7.89 4.1e-07
2026-10-18 09:07:03 YAOGAN-36 05A
NORAD 57452
NASBSAT-2
NORAD 67285
3.006 7.89 4.3e-07
2026-10-19 04:38:53 KANOPUS-V 4
NORAD 43181
NASBSAT-2
NORAD 67285
4.155 15.05 9.3e-08
2026-10-19 16:13:05 SCS-01 D
NORAD 63985
NASBSAT-2
NORAD 67285
3.540 0.20 3.5e-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