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OTTER

In orbit NORAD 66680 XEOD-9474-3581-0595-2203

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

38

Observations all time

Mission information
Spacecraft name
OTTER
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
2025-11-28 18:44:30
Separation time
2025-11-28 19:40:51
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
499.15 km
Apogee
504.96 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6880.2 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 66680U 25276Q   26287.13284822  .00005181  00000-0  24193-3 0  9990
2 66680 97.4092 358.4266 0004220 311.8659 48.2216 15.20248034 48479
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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
2026-10-16 04:09:27 JILIN-1 GAOFEN 2B
NORAD 44836
LEMUR-2-DEANANDMAEVE
NORAD 66680
1.801 0.01 1.3e-06
2026-10-16 11:50:12 LEMUR-2-DEANANDMAEVE
NORAD 66680
IRIDIUM 33 DEB
NORAD 46971
3.217 15.19 1.4e-07
2026-10-18 01:44:35 LEMUR-2-DEANANDMAEVE
NORAD 66680
COSMOS 2251 DEB
NORAD 34451
3.745 15.09 1.1e-07
2026-10-18 03:19:19 LEMUR-2-DEANANDMAEVE
NORAD 66680
COSMOS 2251 DEB
NORAD 34451
4.827 15.09 6.7e-08
2026-10-18 15:47:20 LEMUR-2-DEANANDMAEVE
NORAD 66680
FLOCK 4H-36
NORAD 66739
2.460 0.10 7.3e-07
2026-10-18 17:44:28 FGN-100-D2
NORAD 66299
LEMUR-2-DEANANDMAEVE
NORAD 66680
4.172 14.42 1.1e-07
2026-10-18 18:56:12 PULSAR-0
NORAD 64541
LEMUR-2-DEANANDMAEVE
NORAD 66680
4.075 5.45 2.5e-07
2026-10-18 21:22:08 LEMUR-2-DEANANDMAEVE
NORAD 66680
VIREON-2
NORAD 68421
3.664 12.68 2.0e-07
2026-10-19 02:57:20 LEMUR-2-DEANANDMAEVE
NORAD 66680
CP5
NORAD 38763
3.780 11.73 2.1e-07
2026-10-19 14:07:55 KANOPUS-V 3
NORAD 43180
LEMUR-2-DEANANDMAEVE
NORAD 66680
2.812 15.01 2.0e-07
2026-10-20 23:50:45 LEMUR-2-DEANANDMAEVE
NORAD 66680
PEGASUS DEB
NORAD 24091
3.456 13.24 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