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COSMO

In orbit NORAD 68460 WCPQ-5521-7260-2374-6877 United States of America

Time in UTC

15.10 10:00

Scheduled · Сампо-400 [R1NAV]

112

Observations over 30 days

87%

Successful observations

72k

Frames, latest 2026-10-15 02:27 UTC

Mission information
Spacecraft name
COSMO
Other names
Compact Spaceborne Magnetic Observatory
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-03-29 00:00:00
Separation time
Last observers
Observer
Time of receipt
2026-10-15 02:27:36 UTC
2026-10-15 00:53:15 UTC
2026-10-14 11:59:56 UTC
2026-10-14 10:25:54 UTC
2026-10-14 02:45:25 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
497.75 km
Apogee
507.22 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6880.6 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68460U 26067AW  26287.15760504  .00014001  00000-0  65010-3 0  9999
2 68460 97.4638 243.8830 0006879 33.5516 326.6154 15.20107224 29994
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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
2026-10-15 20:16:50 SPACEMOBILE-002
NORAD 61048
COSMO
NORAD 68460
3.720 13.58 1.7e-07
2026-10-15 21:51:35 SPACEMOBILE-002
NORAD 61048
COSMO
NORAD 68460
3.460 13.60 2.0e-07
2026-10-16 01:35:21 VSP RF A1
NORAD 59135
COSMO
NORAD 68460
3.723 15.10 1.1e-07
2026-10-16 05:24:15 STARLINK-5012
NORAD 53918
COSMO
NORAD 68460
2.291 14.47 1.1e-05
2026-10-16 12:57:27 COSMO
NORAD 68460
PEGASUS DEB
NORAD 24082
2.522 5.43 6.5e-07
2026-10-16 13:47:22 KOYOH
NORAD 58464
COSMO
NORAD 68460
3.982 12.70 1.7e-07
2026-10-16 15:35:40 AAC-HSI-SAT2
NORAD 56995
COSMO
NORAD 68460
2.633 14.87 2.5e-07
2026-10-16 16:56:53 ALISIO-1
NORAD 58562
COSMO
NORAD 68460
4.584 12.77 1.3e-07
2026-10-16 17:10:26 AAC-HSI-SAT2
NORAD 56995
COSMO
NORAD 68460
3.586 14.87 1.3e-07
2026-10-16 18:07:23 OBJECT E
NORAD 63295
COSMO
NORAD 68460
1.432 15.09 7.7e-07
2026-10-17 07:10:50 AAC-HSI-SAT3
NORAD 58848
COSMO
NORAD 68460
4.824 11.42 1.3e-07
2026-10-17 10:56:32 COSMO
NORAD 68460
HULIANWANG JISHU SHIYAN 9B
NORAD 68832
3.700 7.22 2.9e-07
2026-10-17 12:34:55 SPACEMOBILE-006
NORAD 67232
COSMO
NORAD 68460
2.773 12.87 3.5e-07
2026-10-17 13:18:46 COSMO
NORAD 68460
HULIANWANG JISHU SHIYAN 9B
NORAD 68832
1.066 7.24 3.5e-06
2026-10-17 13:22:17 SPACEMOBILE-006
NORAD 67232
COSMO
NORAD 68460
3.419 12.84 2.3e-07
2026-10-17 21:13:50 COSMO
NORAD 68460
CZ-4B DEB
NORAD 43430
3.497 11.51 2.5e-07
2026-10-18 01:20:02 FLOCK 4H-6
NORAD 66709
COSMO
NORAD 68460
3.987 12.75 1.7e-07
2026-10-18 01:27:57 COSMO
NORAD 68460
SL-8 DEB
NORAD 16867
4.387 9.38 1.9e-07
2026-10-18 14:35:46 SPACEMOBILE-002
NORAD 61048
COSMO
NORAD 68460
2.538 14.17 3.3e-07
2026-10-18 21:52:13 BLACK KITE-1
NORAD 66741
COSMO
NORAD 68460
3.088 12.75 2.8e-07
2026-10-19 19:08:31 OBJECT AK
NORAD 57037
COSMO
NORAD 68460
4.063 14.46 1.2e-07
2026-10-20 14:01:18 STARLINK-1522
NORAD 46027
COSMO
NORAD 68460
1.809 9.25 3.3e-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