OTTER, 62623
Orbit data source: Space-Track
OTTER, 62623 is a payload satellite owned by USN PGS (US) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62623 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
USN PGS
Mission
Operational Defense Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 OTTER
1 62623U 25009Q 26080.18361031 .00011893 00000-0 43691-3 0 9992
2 62623 97.4055 162.7713 0003466 254.0751 106.0107 15.28064821 65475Epoch: 2026-03-21T04:24Z
TLE epoch observation values (Epoch: 2026-03-21T04:24:23.930Z)
Latitude
-0.00001°
Longitude
-82.03638°
Altitude
485.356 km
Speed
7.622 km/s
True Right ascension
10h 51m 05s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
05:10:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.929 km
Perigee altitude
476.176 km
Semi-major axis
6,856.69 km
Eccentricity
0.00035
Inclination
97.4055°
RAAN
162.7713°
Arg. of periapsis
254.0751°
True anomaly
106.04887°
Mean anomaly
106.0107°
Eccentric anomaly
106.02979°
Mean motion
3.82271 °/min
Orbital period
94.17 mins
BSTAR
0.00043691
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OTTER Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-22 05:40:20.839Z | 178.93° S | 2026-03-22 05:43:20.839Z | 238.943° WSW | 40.7° | 2026-03-22 05:46:20.839Z | 338.26° N |
| 4 mins | 2026-03-22 18:42:20.839Z | 339.568° N | 2026-03-22 18:43:20.839Z | 309.309° NW | 32.967° | 2026-03-22 18:46:20.839Z | 219.197° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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