ORBASTRO-PC-1, 58258
Orbit data source: Space-Track
ORBASTRO-PC-1, 58258 is a payload satellite owned by OrbAstro (UK) in SSO that was launched on Sat, 11 Nov 2023 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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58258 intel report (Beta)
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Edit Public Description
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 + 2 Pan, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ORBASTRO-PC-1
1 58258U 23174C 25289.18158977 .00025725 00000-0 72485-3 0 9997
2 58258 97.4013 6.9031 0007439 338.3993 21.6936 15.36393080107850Epoch: 2025-10-16T04:21Z
TLE epoch observation values (Epoch: 2025-10-16T04:21:29.356Z)
Latitude
-0.00001°
Longitude
-83.41421°
Altitude
455.174 km
Speed
7.642 km/s
True Right ascension
00h 27m 36s
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
08:18:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.812 km
Perigee altitude
448.647 km
Semi-major axis
6,831.867 km
Eccentricity
0.00074
Inclination
97.4013°
RAAN
6.9031°
Arg. of periapsis
338.3993°
True anomaly
21.72514°
Mean anomaly
21.6936°
Eccentric anomaly
21.70937°
Mean motion
3.84356 °/min
Orbital period
93.66 mins
BSTAR
0.00072485
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Other satellites on launch #174 in the year 2023 (2023-11-11 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-PC-1 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 | 2025-10-16 17:26:36.764Z | 54.718° ENE | 2025-10-16 17:28:36.764Z | 98.742° ESE | 19.554° | 2025-10-16 17:30:36.764Z | 139.842° SSE |
| 5 mins | 2025-10-17 05:30:36.764Z | 182.202° SSW | 2025-10-17 05:32:36.764Z | 282.771° WNW | 41.947° | 2025-10-17 05:35:36.764Z | 341.83° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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