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CSC-1

In orbit NORAD 58022 CNPX-5092-5371-0749-4265 Netherlands

Time in UTC

12.10 17:29

Scheduled · Сампо-400 [R1NAV]

261

Observations over 30 days

43%

Successful observations

377k

Frames, latest 2026-10-12 09:54 UTC

Mission information
Spacecraft name
CSC-1
Other names
CubeSat Carrier-1, ISISpace IOD-1
Status
Active
The satellite is in orbit
Launch and timeline
Launch time
2023-10-07 01:36:00
Separation time
Last observers
Observer
Time of receipt
2026-10-12 09:54:52 UTC
2026-10-12 08:17:55 UTC
2026-10-11 19:24:08 UTC
2026-10-11 17:49:10 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
523.68 km
Apogee
534.10 km
Inclination
97.5°
Period
95.3 min
Semi-major axis
6907.0 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:35 UTC
Two-line elements (TLE)
1 58022U 23155G   26284.92572672  .00006529  00000-0  38990-3 0  9999
2 58022 97.5255 352.6186 0007599 188.4431 171.6672 15.11418463165367
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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
2026-10-13 02:14:46 STARLINK-3328
NORAD 50832
CSC-1
NORAD 58022
1.608 9.84 4.1e-05
2026-10-13 09:32:18 CSC-1
NORAD 58022
OBJECT K
NORAD 42834
3.271 10.67 3.1e-07
2026-10-13 18:38:10 STARLINK-4513
NORAD 53548
CSC-1
NORAD 58022
4.099 14.64 3.3e-06
2026-10-15 04:41:21 OBJECT B
NORAD 56732
CSC-1
NORAD 58022
2.788 12.42 3.6e-07
2026-10-15 07:37:26 CSC-1
NORAD 58022
OBJECT D
NORAD 63294
3.603 8.99 2.8e-07
2026-10-15 11:35:43 CSC-1
NORAD 58022
OBJECT D
NORAD 63294
4.950 8.98 1.5e-07
2026-10-15 11:49:44 CSC-1
NORAD 58022
GRBBETA
NORAD 60237
1.070 14.68 1.6e-06
2026-10-15 21:24:57 STARLINK-4504
NORAD 53555
CSC-1
NORAD 58022
3.380 14.46 5.1e-06
2026-10-17 03:34:32 STARLINK-4495
NORAD 53552
CSC-1
NORAD 58022
2.115 14.29 1.4e-05
2026-10-17 09:00:41 CSC-1
NORAD 58022
ATLAS 5 CENTAUR R/B
NORAD 40978
1.289 12.75 1.6e-06
2026-10-18 01:23:40 AAC-HSI-SAT1
NORAD 56225
CSC-1
NORAD 58022
0.956 14.91 1.8e-06
2026-10-18 02:34:15 STARLINK-3621
NORAD 51769
CSC-1
NORAD 58022
2.711 8.89 1.5e-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