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: 11 hours ago
TLE from 11 hours ago
0 OTP-2
1 63235U 25052AB 25298.27386818 .00004923 00000-0 23117-3 0 9997
2 63235 97.4085 189.4491 0004806 270.7034 89.3650 15.20077263 34136Epoch: 2025-10-25T06:34Z
TLE epoch observation values (Epoch: 2025-10-25T06:34:22.210Z)
Latitude
-0.00009°
Longitude
56.94979°
Altitude
508.663 km
Speed
7.61 km/s
True Right ascension
12h 37m 47s
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
12:39:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.88 km
Perigee altitude
499.266 km
Semi-major axis
6,880.71 km
Eccentricity
0.00048
Inclination
97.4085°
RAAN
189.4491°
Arg. of periapsis
270.7034°
True anomaly
89.42007°
Mean anomaly
89.365°
Eccentric anomaly
89.39253°
Mean motion
3.80271 °/min
Orbital period
94.67 mins
BSTAR
0.00023117
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-25 17:45:41.555Z | 220.767° SW | 2025-10-25 17:47:41.555Z | 255.607° W | 18.288° | 2025-10-25 17:50:41.555Z | 311.699° NW |
| 5 mins | 2025-10-26 05:16:41.555Z | 46.224° ENE | 2025-10-26 05:18:41.555Z | 105.686° ESE | 30.08° | 2025-10-26 05:21:41.555Z | 164.381° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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