Showing default

OTP-2, 63235

Orbit data source: Space-Track

OTP-2, 63235 is a payload satellite owned by Rogue Space (US) in SSO that was launched on Sat, 15 Mar 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
63235, 2025-052AB
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Rogue Space
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
11 kg wet, 11 kg dry
Launch date (UTC)
2025-03-15 (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, 0.3 m
Radar Cross Section
0.055 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 22 hours ago

TLE from 22 hours ago
0 OTP-2
1 63235U 25052AB  26259.46071318  .00008299  00000-0  33452-3 0  9995
2 63235  97.3719 150.5324 0005628 183.4564 176.6636 15.25068432 83775
Epoch: 2026-09-16T11:03Z
TLE epoch observation values (Epoch: 2026-09-16T11:03:25.618Z)
Latitude
-0.00004°
Longitude
-10.73632°
Altitude
497.538 km
Speed
7.614 km/s
True Right ascension
10h 02m 07s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
02:02:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.402 km
Perigee altitude
483.674 km
Semi-major axis
6,865.675 km
Eccentricity
0.00056
Inclination
97.3719°
RAAN
150.5324°
Arg. of periapsis
183.4564°
True anomaly
176.66735°
Mean anomaly
176.6636°
Eccentric anomaly
176.66548°
Mean motion
3.81521 °/min
Orbital period
94.36 mins
BSTAR
0.00033452
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
|