SPIRIT, 58468 (Decayed)
Orbit data source: Space-Track
SPIRIT, 58468 was a payload satellite owned by U Melb. (AU) in LEO 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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Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
U Melb.
Mission
Decayed 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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 SPIRIT
1 58468U 23185G 26213.60561876 .06744580 24838-5 47046-3 0 9991
2 58468 97.3119 302.7880 0014157 311.8558 48.1532 16.39916138149835Epoch: 2026-08-01T14:32Z
TLE epoch observation values (Epoch: 2026-08-01T14:32:05.460Z)
Latitude
-0.00009°
Longitude
134.55023°
Altitude
163.104 km
Speed
7.812 km/s
True Right ascension
20h 11m 09s
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
18:03:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
172.089 km
Perigee altitude
153.569 km
Semi-major axis
6,540.966 km
Eccentricity
0.00142
Inclination
97.3119°
RAAN
302.788°
Arg. of periapsis
311.8558°
True anomaly
48.27419°
Mean anomaly
48.1532°
Eccentric anomaly
48.21368°
Mean motion
4.1028 °/min
Orbital period
87.74 mins
BSTAR
0.00047046
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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
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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. |
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| This satellite is decayed. |
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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