SPIRIT, 58468
Orbit data source: Space-Track
SPIRIT, 58468 is a payload satellite owned by U Melb. (AU) in SSO that was launched on Fri, 01 Dec 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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58468 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
U Melb.
Mission
Operational Amateur Astronomy
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
11.5 kg wet, 11.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 SPIRIT
1 58468U 23185G 25306.50803806 .00038760 00000-0 76414-3 0 9995
2 58468 97.3609 18.0929 0006015 287.9431 72.1163 15.47085326107191Epoch: 2025-11-02T12:11Z
TLE epoch observation values (Epoch: 2025-11-02T12:11:34.488Z)
Latitude
-0.00001°
Longitude
153.17644°
Altitude
427.131 km
Speed
7.656 km/s
True Right ascension
01h 12m 22s
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
23:58:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
426.276 km
Perigee altitude
418.095 km
Semi-major axis
6,800.323 km
Eccentricity
0.0006
Inclination
97.3609°
RAAN
18.0929°
Arg. of periapsis
287.9431°
True anomaly
72.18191°
Mean anomaly
72.1163°
Eccentric anomaly
72.1491°
Mean motion
3.87034 °/min
Orbital period
93.02 mins
BSTAR
0.00076414
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Other satellites on launch #185 in the year 2023 (2023-12-01 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.SPIRIT 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 | 2025-11-03 05:23:32.914Z | 196.396° SSW | 2025-11-03 05:26:32.914Z | 274.789° WNW | 28.883° | 2025-11-03 05:28:32.914Z | 323.174° NNW |
| 5 mins | 2025-11-03 18:14:32.914Z | 348.062° N | 2025-11-03 18:16:32.914Z | 304.062° NW | 27.989° | 2025-11-03 18:19:32.914Z | 223.72° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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