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: 8 hours ago
TLE from 8 hours ago
0 OTP-2
1 63235U 25052AB 25312.42568690 .00007633 00000-0 35356-3 0 9990
2 63235 97.4073 203.3526 0005572 204.0182 156.0794 15.20364151 36287Epoch: 2025-11-08T10:12Z
TLE epoch observation values (Epoch: 2025-11-08T10:12:59.348Z)
Latitude
-0.00003°
Longitude
2.24984°
Altitude
511.339 km
Speed
7.606 km/s
True Right ascension
13h 33m 24s
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
14:05:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.54 km
Perigee altitude
497.873 km
Semi-major axis
6,879.844 km
Eccentricity
0.00056
Inclination
97.4073°
RAAN
203.3526°
Arg. of periapsis
204.0182°
True anomaly
156.10527°
Mean anomaly
156.0794°
Eccentric anomaly
156.09234°
Mean motion
3.80343 °/min
Orbital period
94.65 mins
BSTAR
0.00035356
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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 | 2025-11-09 05:43:39.589Z | 12.117° NNE | 2025-11-09 05:46:39.589Z | 14.721° NNE | 43.3° | 2025-11-09 05:50:39.589Z | 192.721° SSW |
| 5 mins | 2025-11-09 16:22:39.589Z | 124.396° SE | 2025-11-09 16:24:39.589Z | 74.547° E | 28.219° | 2025-11-09 16:27:39.589Z | 10.937° NNE |
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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