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CO3D1

In orbit NORAD 64903 LKTK-5000-8209-9990-7948 France

2025

Launch

0

Observations all time

Mission information
Spacecraft name
CO3D1
Other names
2025-156E
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
2025-06-23 00:00:00
Separation time
2025-06-23 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
501.31 km
Apogee
503.10 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6880.3 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:59 UTC
Two-line elements (TLE)
1 64903U 25156E   26283.54193673  .00003410  00000-0  16059-3 0  9992
2 64903 97.4349 0.4759 0001313 96.2091 263.9294 15.20200725 67057
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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
2026-10-11 02:52:59 CO3D 1
NORAD 64903
VIGORIDE-7
NORAD 68473
4.965 12.98 1.1e-07
2026-10-11 13:09:09 CO3D 1
NORAD 64903
HOTSAT-2
NORAD 68465
4.836 13.09 1.1e-07
2026-10-12 01:44:06 CO3D 1
NORAD 64903
BLACK KITE-1
NORAD 66741
3.480 0.64 3.6e-07
2026-10-12 01:51:43 CO3D 1
NORAD 64903
LANDSAT 5
NORAD 14780
4.467 14.68 5.6e-07
2026-10-12 04:09:36 CO3D 1
NORAD 64903
AEPEX
NORAD 68506
2.020 13.03 6.4e-07
2026-10-12 04:56:59 CO3D 1
NORAD 64903
AEPEX
NORAD 68506
4.812 13.06 1.1e-07
2026-10-12 05:44:22 CO3D 1
NORAD 64903
AEPEX
NORAD 68506
2.681 13.03 3.6e-07
2026-10-12 06:31:45 CO3D 1
NORAD 64903
AEPEX
NORAD 68506
2.866 13.06 3.2e-07
2026-10-12 11:44:30 CO3D 1
NORAD 64903
TITAN 3C TRANSTAGE DEB
NORAD 1961
4.159 12.36 1.6e-07
2026-10-12 11:58:44 CO3D 1
NORAD 64903
RASSVET-3 16
NORAD 68375
4.983 12.47 1.1e-07
2026-10-13 06:09:28 COSMOS 2538
NORAD 44424
CO3D 1
NORAD 64903
4.555 0.44 2.1e-07
2026-10-13 09:19:47 CO3D 1
NORAD 64903
FOSSASAT-2E24
NORAD 66780
4.941 0.76 1.8e-07
2026-10-13 11:57:39 YAOGAN-39 05C
NORAD 58559
CO3D 1
NORAD 64903
3.068 9.78 3.7e-07
2026-10-13 16:26:19 CO3D 1
NORAD 64903
TRANSPORTER-15 OBJECT L
NORAD 66676
2.372 0.76 7.8e-07
2026-10-13 18:48:29 CO3D 1
NORAD 64903
TRANSPORTER-15 OBJECT L
NORAD 66676
4.276 0.76 2.4e-07
2026-10-14 18:31:54 CO3D 1
NORAD 64903
UNKNOWN
NORAD 270100
2.228 10.06 7.0e-07
2026-10-15 04:45:07 BLACKJACK ACES-2
NORAD 56955
CO3D 1
NORAD 64903
2.858 7.47 4.8e-07
2026-10-15 05:37:01 CO3D 1
NORAD 64903
PARUS-6U1
NORAD 68456
3.201 13.08 2.5e-07
2026-10-16 07:37:48 CO3D 1
NORAD 64903
OBJECT B
NORAD 66054
3.827 1.12 3.0e-07
2026-10-16 09:12:23 CO3D 1
NORAD 64903
TRANSPORTER-15 OBJECT DM
NORAD 66773
4.961 0.64 1.8e-07
2026-10-16 10:45:54 CO3D 1
NORAD 64903
RASSVET-3 9
NORAD 68368
4.247 13.04 1.4e-07
2026-10-16 15:37:09 STARLINK-5862
NORAD 55920
CO3D 1
NORAD 64903
3.398 10.05 9.0e-06
2026-10-16 19:27:30 CO3D 1
NORAD 64903
OBJECT C
NORAD 67748
2.060 6.47 9.5e-07
2026-10-16 21:49:40 CO3D 1
NORAD 64903
OBJECT C
NORAD 67748
4.910 6.45 1.7e-07
2026-10-17 01:49:03 HJ-2E
NORAD 54035
CO3D 1
NORAD 64903
3.410 9.16 3.1e-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