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, 0.2 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 26135.26045850 .00003936 00000-0 16785-3 0 9991
2 63235 97.3912 28.1867 0004404 283.0142 77.0603 15.23501438 64854Epoch: 2026-05-15T06:15Z
TLE epoch observation values (Epoch: 2026-05-15T06:15:03.614Z)
Latitude
-0.00004°
Longitude
61.42732°
Altitude
497.708 km
Speed
7.616 km/s
True Right ascension
01h 52m 44s
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
19:51:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.275 km
Perigee altitude
489.224 km
Semi-major axis
6,870.387 km
Eccentricity
0.00044
Inclination
97.3912°
RAAN
28.1867°
Arg. of periapsis
283.0142°
True anomaly
77.10949°
Mean anomaly
77.0603°
Eccentric anomaly
77.08489°
Mean motion
3.81128 °/min
Orbital period
94.46 mins
BSTAR
0.00016785
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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 | 2026-05-16 17:03:26.310Z | 178.365° S | 2026-05-16 17:06:26.310Z | 278.432° WNW | 42.002° | 2026-05-16 17:09:26.310Z | 341.003° N |
| 5 mins | 2026-05-17 06:06:26.310Z | 351.11° N | 2026-05-17 06:08:26.310Z | 306.021° NW | 33.351° | 2026-05-17 06:11:26.310Z | 219.429° SW |
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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