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OTTER SDM

In orbit NORAD 66678 GFMG-5057-6932-8166-4926

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
OTTER SDM
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
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
496.86 km
Apogee
502.75 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6877.9 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:04 UTC
Two-line elements (TLE)
1 66678U 25276N   26287.17671909  .00005965  00000-0  27205-3 0  9994
2 66678 97.4103 358.7082 0004283 312.4264 47.6609 15.20995453 48491
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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
2026-10-18 00:45:11 OTTER SDM
NORAD 66678
HULIANWANG JISHU SHIYAN 9B
NORAD 68832
3.692 14.53 1.4e-07
2026-10-18 08:28:50 CAS500-1
NORAD 47932
OTTER SDM
NORAD 66678
3.539 15.09 1.3e-07
2026-10-18 10:03:35 CAS500-1
NORAD 47932
OTTER SDM
NORAD 66678
4.295 15.09 8.5e-08
2026-10-18 10:50:58 CAS500-1
NORAD 47932
OTTER SDM
NORAD 66678
2.577 15.10 2.4e-07
2026-10-18 12:25:43 CAS500-1
NORAD 47932
OTTER SDM
NORAD 66678
1.919 15.10 4.3e-07
2026-10-18 14:00:29 CAS500-1
NORAD 47932
OTTER SDM
NORAD 66678
4.431 15.10 8.0e-08
2026-10-19 02:37:25 TOMORROW-S9
NORAD 66309
OTTER SDM
NORAD 66678
0.360 14.41 1.5e-05
2026-10-19 04:21:14 HXMT (HUIYAN)
NORAD 42758
OTTER SDM
NORAD 66678
4.468 14.00 1.1e-07
2026-10-19 05:56:38 YAOGAN-36 03B
NORAD 54374
OTTER SDM
NORAD 66678
4.198 9.58 2.0e-07
2026-10-19 10:29:18 SEMI-1N
NORAD 66297
OTTER SDM
NORAD 66678
3.939 14.35 1.3e-07
2026-10-19 11:22:37 HERMES-1
NORAD 63242
OTTER SDM
NORAD 66678
3.558 15.09 1.2e-07
2026-10-19 12:30:18 OTTER SDM
NORAD 66678
RASSVET-3 8
NORAD 68367
4.816 13.17 1.1e-07
2026-10-19 15:13:31 SEMI-1P
NORAD 66298
OTTER SDM
NORAD 66678
4.164 14.35 1.2e-07
2026-10-19 15:18:53 OTTER SDM
NORAD 66678
IRIDIUM 33 DEB
NORAD 46971
2.258 15.22 2.9e-07
2026-10-19 18:53:28 OTTER SDM
NORAD 66678
DB GME UT (DB-GLOBE MISSION EARTH-UT)
NORAD 68459
4.063 12.72 1.6e-07
2026-10-20 03:31:12 OTTER SDM
NORAD 66678
FLOCK 4H-3
NORAD 66706
4.030 0.04 2.7e-07
2026-10-20 04:18:44 OTTER SDM
NORAD 66678
FLOCK 4H-3
NORAD 66706
2.683 0.04 6.1e-07
2026-10-20 04:49:33 HULIANWANG JISHU SHIYAN 6B
NORAD 63429
OTTER SDM
NORAD 66678
4.207 14.64 1.0e-07
2026-10-20 05:06:03 OTTER SDM
NORAD 66678
FLOCK 4H-3
NORAD 66706
1.867 0.04 1.3e-06
2026-10-20 05:53:11 OTTER SDM
NORAD 66678
FLOCK 4H-3
NORAD 66706
4.227 0.04 2.5e-07
2026-10-20 13:47:32 OTTER SDM
NORAD 66678
ZORKY-2M 7
NORAD 67268
3.186 0.16 4.3e-07
2026-10-21 02:11:25 OTTER SDM
NORAD 66678
COSMOS 886 DEB
NORAD 20673
3.847 15.03 1.1e-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