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: 11 hours ago
TLE from 11 hours ago
0 OTTER
1 62623U 25009Q 26192.72980104 .00005912 00000-0 20419-3 0 9992
2 62623 97.4036 274.7978 0004106 205.3930 154.7110 15.30315772 82673Epoch: 2026-07-11T17:30Z
TLE epoch observation values (Epoch: 2026-07-11T17:30:54.809Z)
Latitude
-0°
Longitude
82.4306°
Altitude
480.519 km
Speed
7.624 km/s
True Right ascension
18h 19m 11s
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
17:11:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.634 km
Perigee altitude
469.009 km
Semi-major axis
6,849.958 km
Eccentricity
0.00041
Inclination
97.4036°
RAAN
274.7978°
Arg. of periapsis
205.393°
True anomaly
154.73109°
Mean anomaly
154.711°
Eccentric anomaly
154.72105°
Mean motion
3.82835 °/min
Orbital period
94.04 mins
BSTAR
0.00020419
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-12 06:11:46.639Z | 208.748° SW | 2026-07-12 06:14:46.639Z | 275.208° WNW | 23.233° | 2026-07-12 06:16:46.639Z | 315.798° NNW |
| 4 mins | 2026-07-12 17:38:46.639Z | 63.539° ENE | 2026-07-12 17:39:46.639Z | 85.494° E | 19.176° | 2026-07-12 17:42:46.639Z | 144.924° SSE |
| 4 mins | 2026-07-12 19:11:46.639Z | 324.031° NNW | 2026-07-12 19:13:46.639Z | 278.359° WNW | 18.883° | 2026-07-12 19:15:46.639Z | 242.657° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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