Showing default

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.

Loading next visibility...
Identifier
62623, 2025-009Q
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
USN PGS
Mission
Operational Defense Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2025-01-14 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 OTTER
1 62623U 25009Q   26238.22925750  .00008189  00000-0  27545-3 0  9990
2 62623  97.4002 320.1673 0005972  70.6980 289.4906 15.31043988 89634
Epoch: 2026-08-26T05:30Z
TLE epoch observation values (Epoch: 2026-08-26T05:30:07.847Z)
Latitude
-0.00011°
Longitude
-96.85063°
Altitude
474.439 km
Speed
7.629 km/s
True Right ascension
21h 20m 40s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
04:37:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.737 km
Perigee altitude
465.558 km
Semi-major axis
6,847.784 km
Eccentricity
0.0006
Inclination
97.4002°
RAAN
320.1673°
Arg. of periapsis
70.698°
True anomaly
289.42607°
Mean anomaly
289.4906°
Eccentric anomaly
289.45834°
Mean motion
3.83017 °/min
Orbital period
93.99 mins
BSTAR
0.00027545
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|