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RANDEV

In orbit NORAD 52898 LYKB-5376-2648-5150-0020 South Korea

Time in UTC

03:43

Next pass · ИТ-куб, Калининград · 2°

—

No observations scheduled

1

Observations over 30 days

73%

Successful observations

5k

Frames, latest 2026-10-12 14:19 UTC

Mission information
Spacecraft name
RANDEV
Other names
ASTRIS 2
Frequency usage status
Violator
Status
Active
The satellite is in orbit
Launch and timeline
Launch time
2022-06-21 07:00:00
Separation time
2022-06-01 09:36:00
Last observers
Observer
Time of receipt
2026-10-12 14:19:18 UTC
2026-08-29 15:29:16 UTC
2026-08-26 16:50:13 UTC
2026-08-26 15:15:44 UTC
2025-08-18 05:53:00 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
671.87 km
Apogee
683.87 km
Inclination
98.2°
Period
98.4 min
Semi-major axis
7056.0 km
Velocity
7.52 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 22:09:12 UTC
Two-line elements (TLE)
1 52898U 22065E   26286.60026597  .00001023  00000-0  20514-3 0  9997
2 52898 98.2385 70.6760 0008405 22.6895 337.4678 14.63847517228572
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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 15:55:50 AURA
NORAD 28376
RANDEV
NORAD 52898
4.764 14.83 7.1e-08
2026-10-16 07:33:09 RANDEV
NORAD 52898
COSMOS 2251 DEB
NORAD 36540
3.997 13.07 1.6e-07
2026-10-16 16:11:06 RANDEV
NORAD 52898
IRIDIUM 33 DEB
NORAD 34521
1.467 15.02 6.9e-07
2026-10-16 21:41:10 RANDEV
NORAD 52898
FENGYUN 1C DEB
NORAD 32304
2.403 14.28 3.4e-07
2026-10-16 23:17:04 RANDEV
NORAD 52898
DELTA 1 DEB
NORAD 13571
3.473 13.66 1.9e-07
2026-10-17 03:13:43 SWISSCUBE
NORAD 35932
RANDEV
NORAD 52898
4.328 13.21 1.3e-07
2026-10-17 05:00:24 RANDEV
NORAD 52898
COSMOS 2251 DEB
NORAD 40810
4.898 13.75 9.3e-08
2026-10-17 11:13:18 RANDEV
NORAD 52898
SL-16 DEB
NORAD 22339
3.639 14.97 1.2e-07
2026-10-18 06:11:50 RANDEV
NORAD 52898
COSMOS 2251 DEB
NORAD 36385
2.651 14.92 2.2e-07
2026-10-18 06:50:46 RANDEV
NORAD 52898
COSMOS 2251 DEB
NORAD 34680
4.926 14.98 6.2e-08
2026-10-18 09:41:19 VNREDSAT 1
NORAD 39160
RANDEV
NORAD 52898
4.241 11.02 1.8e-07
2026-10-18 12:24:45 RANDEV
NORAD 52898
ORBCOMM FM115
NORAD 41186
3.800 14.16 1.4e-07
2026-10-18 13:12:18 RANDEV
NORAD 52898
FENGYUN 1C DEB
NORAD 31342
3.395 14.84 1.4e-07
2026-10-18 18:30:51 RANDEV
NORAD 52898
COSMOS 886 DEB
NORAD 9649
3.925 7.53 2.5e-07
2026-10-18 20:11:08 RANDEV
NORAD 52898
COSMOS 2251 DEB
NORAD 33940
3.478 14.84 1.3e-07
2026-10-19 18:35:08 RANDEV
NORAD 52898
COSMOS 886 DEB
NORAD 9953
4.697 9.33 1.6e-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