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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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: 6 hours ago
TLE from 6 hours ago
0 ORBASTRO-PC-1
1 58258U 23174C 26130.82925905 .00015171 00000-0 30181-3 0 9998
2 58258 97.3768 216.1142 0004916 307.0929 52.9871 15.47020984139697Epoch: 2026-05-10T19:54Z
TLE epoch observation values (Epoch: 2026-05-10T19:54:07.981Z)
Latitude
-0.00006°
Longitude
48.95423°
Altitude
426.561 km
Speed
7.657 km/s
True Right ascension
14h 24m 27s
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
10:18:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
425.718 km
Perigee altitude
419.032 km
Semi-major axis
6,800.512 km
Eccentricity
0.00049
Inclination
97.3768°
RAAN
216.1142°
Arg. of periapsis
307.0929°
True anomaly
53.0321°
Mean anomaly
52.9871°
Eccentric anomaly
53.0096°
Mean motion
3.87018 °/min
Orbital period
93.02 mins
BSTAR
0.00030181
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-11 05:21:30.099Z | 137.723° SSE | 2026-05-11 05:23:30.099Z | 82.167° E | 32.442° | 2026-05-11 05:26:30.099Z | 4.69° NNE |
| 5 mins | 2026-05-11 18:12:30.099Z | 36.429° NE | 2026-05-11 18:14:30.099Z | 102.451° ESE | 33.346° | 2026-05-11 18:17:30.099Z | 171.342° S |
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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