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TOM-3

In orbit NORAD 69906 HWNI-0814-4699-2907-4799 Germany

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

6

Observations all time

Mission information
Spacecraft name
TOM-3
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
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-07-07 07:12:00
Separation time
2026-07-07 08:08:33
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
588.70 km
Apogee
594.93 km
Inclination
97.7°
Period
96.6 min
Semi-major axis
6970.0 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:21 UTC
Two-line elements (TLE)
1 69906U 26156AP  26282.96878059  .00000936  00000-0  10025-3 0  9991
2 69906 97.7373 181.6359 0004473 153.8885 206.2560 14.91005776 14104
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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 00:35:18 SJ-9B
NORAD 38861
TOM-3
NORAD 69906
3.527 9.75 2.8e-07
2026-10-11 05:31:22 TOM-3
NORAD 69906
FENGYUN 1C DEB
NORAD 31443
2.898 13.33 2.9e-07
2026-10-11 21:32:11 IO-1
NORAD 68498
TOM-3
NORAD 69906
3.402 7.22 3.4e-07
2026-10-12 04:48:14 ICEYE-X78
NORAD 68995
TOM-3
NORAD 69906
4.654 0.45 2.0e-07
2026-10-12 05:36:32 ICEYE-X78
NORAD 68995
TOM-3
NORAD 69906
2.127 0.45 9.8e-07
2026-10-13 00:05:30 UMBRA-12
NORAD 67371
TOM-3
NORAD 69906
2.952 11.37 3.6e-07
2026-10-13 00:34:58 FIREFLY-3
NORAD 62710
TOM-3
NORAD 69906
4.620 14.98 7.4e-08
2026-10-13 02:02:13 TOM-3
NORAD 69906
CBERS 1 DEB
NORAD 35387
4.969 14.95 6.5e-08
2026-10-13 02:11:33 FIREFLY-3
NORAD 62710
TOM-3
NORAD 69906
3.094 14.98 1.6e-07
2026-10-13 03:38:49 TOM-3
NORAD 69906
CBERS 1 DEB
NORAD 35387
0.334 14.95 1.4e-05
2026-10-13 13:07:19 IRIDE-MS2-HEO-9
NORAD 64585
TOM-3
NORAD 69906
3.399 14.32 1.7e-07
2026-10-13 15:46:40 TOM-3
NORAD 69906
CZ-6A DEB
NORAD 54629
4.953 14.97 6.5e-08
2026-10-14 10:26:46 FFLY03
NORAD 65319
TOM-3
NORAD 69906
4.962 14.96 6.4e-08
2026-10-15 06:52:28 SERT3
NORAD 68499
TOM-3
NORAD 69906
4.724 7.25 1.8e-07
2026-10-15 12:37:43 BB4
NORAD 57757
TOM-3
NORAD 69906
3.858 5.59 2.8e-07
2026-10-16 06:55:16 TOM-3
NORAD 69906
CZ-4B DEB
NORAD 39052
4.264 14.50 1.0e-07
2026-10-16 14:18:01 FOREST-17 (TELPERION)
NORAD 68988
TOM-3
NORAD 69906
3.822 0.46 3.0e-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