ORBASTRO-TR5, 63236
Orbit data source: Space-Track
ORBASTRO-TR5, 63236 is a UK payload satellite 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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63236 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
OrbAstro
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 ORBASTRO-TR5
1 63236U 25052AC 26206.49000016 .00004641 00000-0 20410-3 0 9995
2 63236 97.3791 97.4603 0004925 43.0776 317.0845 15.22360940 75646Epoch: 2026-07-25T11:45Z
TLE epoch observation values (Epoch: 2026-07-25T11:45:36.013Z)
Latitude
-0.00006°
Longitude
-22.14128°
Altitude
499.336 km
Speed
7.616 km/s
True Right ascension
06h 29m 50s
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
18:17:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.068 km
Perigee altitude
492.298 km
Semi-major axis
6,873.82 km
Eccentricity
0.00049
Inclination
97.3791°
RAAN
97.4603°
Arg. of periapsis
43.0776°
True anomaly
317.04605°
Mean anomaly
317.0845°
Eccentric anomaly
317.06528°
Mean motion
3.80843 °/min
Orbital period
94.53 mins
BSTAR
0.0002041
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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.ORBASTRO-TR5 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 | 2026-07-26 05:39:50.779Z | 11.155° NNE | 2026-07-26 05:43:50.779Z | 199.739° SSW | 42.8° | 2026-07-26 05:46:50.779Z | 194.014° SSW |
| 4 mins | 2026-07-26 16:18:50.779Z | 114.688° SE | 2026-07-26 16:19:50.779Z | 87.863° E | 27.298° | 2026-07-26 16:22:50.779Z | 14.022° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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