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, 0.2 m
Radar Cross Section
0.055 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 OTP-2
1 63235U 25052AB 26032.48296286 .00003430 00000-0 15444-3 0 9992
2 63235 97.4044 287.0067 0004767 286.1402 73.9309 15.21732508 49217Epoch: 2026-02-01T11:35Z
TLE epoch observation values (Epoch: 2026-02-01T11:35:27.991Z)
Latitude
-0.00001°
Longitude
-18.55189°
Altitude
502.801 km
Speed
7.613 km/s
True Right ascension
19h 08m 01s
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
05:38:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.856 km
Perigee altitude
494.3 km
Semi-major axis
6,875.715 km
Eccentricity
0.00048
Inclination
97.4044°
RAAN
287.0067°
Arg. of periapsis
286.1402°
True anomaly
73.9834°
Mean anomaly
73.9309°
Eccentric anomaly
73.95715°
Mean motion
3.80686 °/min
Orbital period
94.57 mins
BSTAR
0.00015444
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-02 05:30:59.216Z | 22.016° NNE | 2026-02-02 05:33:59.216Z | 107.67° ESE | 40.775° | 2026-02-02 05:36:59.216Z | 179.523° S |
| 4 mins | 2026-02-02 17:42:59.216Z | 227.942° WSW | 2026-02-02 17:44:59.216Z | 270.315° WNW | 19.452° | 2026-02-02 17:46:59.216Z | 308.483° NW |
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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