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.
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63235 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Rogue Space
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
11 kg wet, 11 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.055 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OTP-2
1 63235U 25052AB 25259.95322274 .00008881 00000-0 42384-3 0 9999
2 63235 97.4133 151.8185 0008669 51.7569 308.4445 15.19262711 28316Epoch: 2025-09-16T22:52Z
TLE epoch observation values (Epoch: 2025-09-16T22:52:38.444Z)
Latitude
-0°
Longitude
172.52219°
Altitude
507.447 km
Speed
7.612 km/s
True Right ascension
10h 07m 16s
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
16:50:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.002 km
Perigee altitude
499.068 km
Semi-major axis
6,883.172 km
Eccentricity
0.00087
Inclination
97.4133°
RAAN
151.8185°
Arg. of periapsis
51.7569°
True anomaly
308.36664°
Mean anomaly
308.4445°
Eccentric anomaly
308.40558°
Mean motion
3.80067 °/min
Orbital period
94.72 mins
BSTAR
0.00042384
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.OTP-2 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-18 05:28:05.439Z | 22.512° NE | 2025-09-18 05:31:05.439Z | 71.519° E | 37.08° | 2025-09-18 05:35:05.439Z | 177.608° S |
| 4 mins | 2025-09-18 16:08:05.439Z | 105.865° ESE | 2025-09-18 16:10:05.439Z | 62.681° ENE | 19.682° | 2025-09-18 16:12:05.439Z | 25.3° NE |
| 4 mins | 2025-09-18 17:42:05.439Z | 230.572° WSW | 2025-09-18 17:44:05.439Z | 276.984° WNW | 20.276° | 2025-09-18 17:46:05.439Z | 313.094° NW |
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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