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Otter Pup 2

In orbit NORAD 64537 TNIF-9489-4101-4135-4428

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

65

Observations all time

Mission information
Spacecraft name
Otter Pup 2
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
2025-06-23 21:25:00
Separation time
2025-06-23 22:21:36
Last observers
Observer
Time of receipt
2025-07-09 14:12:04 UTC
2025-07-08 23:41:52 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
489.29 km
Apogee
494.46 km
Inclination
97.5°
Period
94.5 min
Semi-major axis
6870.0 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-06 04:46:20 UTC
Two-line elements (TLE)
1 64537U 25135K   26273.27421420  .00000252  00000-0  13520-4 0  9997
2 64537 97.4854 28.3815 0003768 147.8183 212.3284 15.23627354 70879
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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 10:09:06 SCS-01 K
NORAD 63991
OTTER PUP 2
NORAD 64537
0.865 5.77 5.5e-06
2026-10-11 17:14:51 OBJECT C
NORAD 57426
OTTER PUP 2
NORAD 64537
4.322 6.90 2.1e-07
2026-10-12 05:18:41 STARLINK-5592
NORAD 55741
OTTER PUP 2
NORAD 64537
1.622 4.22 4.9e-05
2026-10-13 12:29:58 TRANSPORTER-13 OBJECT U
NORAD 63228
OTTER PUP 2
NORAD 64537
1.038 13.97 2.0e-06
2026-10-13 19:58:04 STARLINK-5592
NORAD 55741
OTTER PUP 2
NORAD 64537
3.265 3.90 1.2e-05
2026-10-13 23:37:22 OTTER PUP 2
NORAD 64537
FLOCK 4H-2
NORAD 66705
2.211 5.54 8.5e-07
2026-10-14 07:24:59 ORBASTRO-TR5
NORAD 63236
OTTER PUP 2
NORAD 64537
3.558 13.89 1.8e-07
2026-10-14 09:46:52 ORBASTRO-TR5
NORAD 63236
OTTER PUP 2
NORAD 64537
1.071 13.93 2.0e-06
2026-10-14 15:23:05 OTTER PUP 2
NORAD 64537
GENA-OT
NORAD 66774
3.084 5.51 4.4e-07
2026-10-15 06:05:15 STARLINK-3333
NORAD 50805
OTTER PUP 2
NORAD 64537
2.990 14.52 6.6e-06
2026-10-15 11:21:24 YAOGAN-42 01
NORAD 59395
OTTER PUP 2
NORAD 64537
1.549 9.08 1.5e-06
2026-10-16 07:48:42 OTTER PUP 2
NORAD 64537
SEMI-1P
NORAD 66298
0.721 13.92 4.3e-06
2026-10-16 07:58:47 YAOGAN-39 03A
NORAD 57986
OTTER PUP 2
NORAD 64537
3.662 13.93 1.7e-07
2026-10-16 09:23:00 OTTER PUP 2
NORAD 64537
SEMI-1N
NORAD 66297
1.059 13.87 2.0e-06

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