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TOM-2

In orbit NORAD 69914 SKCR-7506-5885-9369-1623 Germany

Observations 6
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2026

Falcon 9 Block 5 | Transporter 17 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

6

Observations all time

Mission information
Spacecraft name
TOM-2
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
Falcon 9 Block 5 | Transporter 17 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-07-07 07:12:00
Separation time
2026-07-07 08:11:41
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
589.78 km
Apogee
594.60 km
Inclination
97.7°
Period
96.6 min
Semi-major axis
6970.3 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:21 UTC
Two-line elements (TLE)
1 69914U 26156AX  26282.44308139  .00000778  00000-0  84486-4 0  9997
2 69914  97.7460 181.1948 0003457 140.8180 219.3289 14.90884908 14029
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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 04:06:35 IRIDE-MS2-HEO-13
NORAD 68985 		TOM-2
NORAD 69914 		3.152 0.46 4.4e-07
2026-10-11 14:21:04 TOM-2
NORAD 69914 		OBJECT F
NORAD 100463 		2.048 14.89 3.9e-07
2026-10-12 03:34:24 IRIDE-MS2-HEO-6
NORAD 64576 		TOM-2
NORAD 69914 		4.475 14.34 9.9e-08
2026-10-12 09:07:34 TOM-2
NORAD 69914 		PEGASUS R/B
NORAD 39198 		2.089 7.78 8.8e-07
2026-10-13 06:24:38 TOM-2
NORAD 69914 		CZ-6A DEB
NORAD 54632 		3.558 14.97 1.3e-07
2026-10-13 08:55:07 BEIJING-3B
NORAD 53587 		TOM-2
NORAD 69914 		3.746 14.98 1.1e-07
2026-10-13 18:54:41 N1-ATLAS
NORAD 68501 		TOM-2
NORAD 69914 		4.811 7.23 1.7e-07
2026-10-14 04:03:39 TOM-2
NORAD 69914 		CZ-6A DEB
NORAD 55208 		4.548 14.91 7.8e-08
2026-10-15 07:39:26 TOM-2
NORAD 69914 		FRAMSAT-1
NORAD 100610 		3.610 14.95 1.2e-07
2026-10-15 11:11:42 TRITON-1
NORAD 39427 		TOM-2
NORAD 69914 		2.635 1.10 6.3e-07
2026-10-15 15:43:55 LEAP-1
NORAD 65321 		TOM-2
NORAD 69914 		4.103 14.95 9.5e-08
2026-10-15 17:20:32 LEAP-1
NORAD 65321 		TOM-2
NORAD 69914 		0.966 14.95 1.7e-06
2026-10-16 12:11:01 ICEYE-X79
NORAD 69870 		TOM-2
NORAD 69914 		4.099 0.01 2.6e-07
2026-10-16 18:36:44 NAVIGATOR
NORAD 69887 		TOM-2
NORAD 69914 		4.530 0.02 2.1e-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