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OTTER

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

Falcon 9

Carrier rocket

База Вандерберг

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
Spaceport
База Вандерберг
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
499.07 km
Apogee
505.39 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6880.4 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:20 UTC
Two-line elements (TLE)
1 66680U 25276Q   26282.45948874  .00003959  00000-0  18591-3 0  9990
2 66680 97.4107 353.8354 0004595 332.2330 27.8659 15.20190345 47767
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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 02:48:33 LEMUR-2-DEANANDMAEVE
NORAD 66680
SL-3 R/B
NORAD 12904
3.037 5.03 1.2e-06
2026-10-11 14:45:41 LEMUR-2-DEANANDMAEVE
NORAD 66680
FLOCK 4H-24
NORAD 66727
3.480 0.06 3.6e-07
2026-10-11 19:49:26 LEMUR-2-DEANANDMAEVE
NORAD 66680
RAVEN
NORAD 69016
4.285 15.08 8.6e-08
2026-10-12 02:43:29 STARLINK-5072
NORAD 55758
LEMUR-2-DEANANDMAEVE
NORAD 66680
4.395 8.30 5.9e-06
2026-10-12 15:58:52 LEMUR-2-DEANANDMAEVE
NORAD 66680
CZ-4C DEB
NORAD 43266
2.850 13.02 3.2e-07
2026-10-12 23:56:47 LEMUR-2-DEANANDMAEVE
NORAD 66680
OBJECT D
NORAD 67251
4.417 0.80 2.3e-07
2026-10-13 05:42:22 LEMUR-2-DEANANDMAEVE
NORAD 66680
SPACEMOBILE-006
NORAD 67232
1.981 14.38 5.1e-07
2026-10-13 19:02:25 LEMUR-2-DEANANDMAEVE
NORAD 66680
COSMOS 2251 DEB
NORAD 33795
3.582 15.06 1.2e-07
2026-10-14 10:41:29 LEMUR-2-DEANANDMAEVE
NORAD 66680
GYEONGGISAT-1
NORAD 66771
4.031 0.12 2.7e-07
2026-10-14 17:20:01 LEMUR-2-DEANANDMAEVE
NORAD 66680
BSLT-3
NORAD 69009
3.296 15.08 1.4e-07
2026-10-15 16:41:37 TPA-1
NORAD 64533
LEMUR-2-DEANANDMAEVE
NORAD 66680
1.013 5.51 4.0e-06
2026-10-15 18:24:06 LEMUR-2-DEANANDMAEVE
NORAD 66680
UNISAT
NORAD 26547
3.014 10.47 1.4e-07
2026-10-16 07:42:51 TIANYI A
NORAD 64048
LEMUR-2-DEANANDMAEVE
NORAD 66680
1.472 0.13 2.0e-06
2026-10-16 11:50:15 LEMUR-2-DEANANDMAEVE
NORAD 66680
IRIDIUM 33 DEB
NORAD 46971
2.388 15.19 2.6e-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