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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ORBASTRO-PC-1
1 58258U 23174C 26234.61571368 .00025068 00000-0 42149-3 0 9993
2 58258 97.3762 322.2315 0004689 274.0519 86.0197 15.51729356155766Epoch: 2026-08-22T14:46Z
TLE epoch observation values (Epoch: 2026-08-22T14:46:37.661Z)
Latitude
-0.00009°
Longitude
129.65102°
Altitude
414.591 km
Speed
7.662 km/s
True Right ascension
21h 28m 55s
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
11:30:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
411.781 km
Perigee altitude
405.417 km
Semi-major axis
6,786.736 km
Eccentricity
0.00047
Inclination
97.3762°
RAAN
322.2315°
Arg. of periapsis
274.0519°
True anomaly
86.0733°
Mean anomaly
86.0197°
Eccentric anomaly
86.0465°
Mean motion
3.88197 °/min
Orbital period
92.74 mins
BSTAR
0.00042149
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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 | 2026-08-23 06:23:16.932Z | 200.531° SSW | 2026-08-23 06:25:16.932Z | 256.954° W | 30.118° | 2026-08-23 06:28:16.932Z | 329.966° NNW |
| 4 mins | 2026-08-23 19:12:16.932Z | 340.35° N | 2026-08-23 19:14:16.932Z | 263.924° W | 29.934° | 2026-08-23 19:16:16.932Z | 220.575° 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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