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STEP CubeLab-II

In orbit NORAD 52897 ODFG-1778-1250-1047-4122 South Korea

2022

Launch

1

Observations all time

Mission information
Spacecraft name
STEP CubeLab-II
Frequency usage status
Violator
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2022-06-21 07:00:00
Separation time
2022-06-29 07:50:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
672.63 km
Apogee
685.66 km
Inclination
98.2°
Period
98.4 min
Semi-major axis
7057.3 km
Velocity
7.5 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:37 UTC
Two-line elements (TLE)
1 52897U 22065D   26283.89587582  .00000483  00000-0  10268-3 0  9994
2 52897 98.2392 67.5682 0009233 29.7808 330.3918 14.63446481228427
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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 00:12:24 STEP CUBE LAB-II
NORAD 52897
SITRO-AIS 28
NORAD 59071
4.882 12.42 1.2e-07
2026-10-12 06:32:56 STEP CUBE LAB-II
NORAD 52897
GLOBALSTAR M105
NORAD 100331
3.107 10.17 3.5e-07
2026-10-12 07:22:08 STEP CUBE LAB-II
NORAD 52897
GLOBALSTAR M105
NORAD 100331
2.953 10.15 3.9e-07
2026-10-12 14:07:36 STEP CUBE LAB-II
NORAD 52897
FENGYUN 1C DEB
NORAD 31427
1.559 1.86 1.8e-06
2026-10-12 14:26:25 STEP CUBE LAB-II
NORAD 52897
UNKNOWN
NORAD 270403
3.014 15.02 1.6e-07
2026-10-12 15:36:30 STEP CUBE LAB-II
NORAD 52897
SL-8 DEB
NORAD 18502
1.130 14.87 1.2e-06
2026-10-13 04:14:30 STEP CUBE LAB-II
NORAD 52897
COSMOS 2251 DEB
NORAD 35022
4.228 4.88 2.4e-07
2026-10-13 05:09:04 STEP CUBE LAB-II
NORAD 52897
COSMOS 2251 DEB
NORAD 34857
4.929 14.98 6.2e-08
2026-10-13 12:15:03 SJ-11-05
NORAD 39202
STEP CUBE LAB-II
NORAD 52897
2.128 5.33 9.2e-07
2026-10-13 18:07:50 STEP CUBE LAB-II
NORAD 52897
CZ-6A DEB
NORAD 60838
2.709 14.88 2.2e-07
2026-10-15 04:29:40 STEP CUBE LAB-II
NORAD 52897
FENGYUN 1C DEB
NORAD 31083
3.594 0.62 3.4e-07
2026-10-15 12:50:44 STEP CUBE LAB-II
NORAD 52897
USA 57
NORAD 20561
4.701 14.90 7.0e-08
2026-10-15 19:23:14 STEP CUBE LAB-II
NORAD 52897
CZ-6A DEB
NORAD 60716
0.959 14.92 1.7e-06
2026-10-15 20:40:21 STEP CUBE LAB-II
NORAD 52897
SL-16 DEB
NORAD 22339
4.324 14.90 8.4e-08
2026-10-16 06:01:48 STEP CUBE LAB-II
NORAD 52897
COSMOS 2251 DEB
NORAD 34726
3.275 6.56 3.8e-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