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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OTP-2
1 63235U 25052AB 26263.65988639 .00005156 00000-0 20872-3 0 9995
2 63235 97.3719 154.6685 0006088 168.7516 191.3859 15.25112179 84415Epoch: 2026-09-20T15:50Z
TLE epoch observation values (Epoch: 2026-09-20T15:50:14.184Z)
Latitude
-0.00002°
Longitude
-82.44148°
Altitude
497.647 km
Speed
7.613 km/s
True Right ascension
10h 18m 40s
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
19:14:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.586 km
Perigee altitude
483.226 km
Semi-major axis
6,865.543 km
Eccentricity
0.00061
Inclination
97.3719°
RAAN
154.6685°
Arg. of periapsis
168.7516°
True anomaly
191.37214°
Mean anomaly
191.3859°
Eccentric anomaly
191.37902°
Mean motion
3.81532 °/min
Orbital period
94.36 mins
BSTAR
0.00020872
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-22 06:12:40.594Z | 331.412° NNW | 2026-09-22 06:13:40.594Z | 301.484° NW | 34.948° | 2026-09-22 06:16:40.594Z | 224.688° SW |
| 5 mins | 2026-09-22 16:47:40.594Z | 157.308° SSE | 2026-09-22 16:49:40.594Z | 81.693° E | 73.356° | 2026-09-22 16:52:40.594Z | 353.117° N |
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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