SPIP, 58298
Orbit data source: Space-Track
SPIP, 58298 is a payload satellite owned by Aerospacelab (BE) 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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58298 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
BE / BELRelated business
Manufacturer
Aerospacelab
Mission
Operational Commercial Imaging
Bus & Motor
VSP, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.963 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 SPIP
1 58298U 23174AU 25349.96311690 .00004328 00000-0 17284-3 0 9999
2 58298 97.4052 63.3074 0011301 111.3309 248.9136 15.25618110116829Epoch: 2025-12-15T23:06Z
TLE epoch observation values (Epoch: 2025-12-15T23:06:53.300Z)
Latitude
-0.00006°
Longitude
-8.26882°
Altitude
494.828 km
Speed
7.616 km/s
True Right ascension
04h 13m 13s
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
14:42:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.645 km
Perigee altitude
478.131 km
Semi-major axis
6,864.025 km
Eccentricity
0.00113
Inclination
97.4052°
RAAN
63.3074°
Arg. of periapsis
111.3309°
True anomaly
248.79283°
Mean anomaly
248.9136°
Eccentric anomaly
248.85321°
Mean motion
3.81658 °/min
Orbital period
94.33 mins
BSTAR
0.00017284
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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.SPIP 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 | 2025-12-16 17:00:39.718Z | 55.914° ENE | 2025-12-16 17:02:39.718Z | 91.084° ESE | 15.183° | 2025-12-16 17:04:39.718Z | 127.888° SE |
| 4 mins | 2025-12-16 18:34:39.718Z | 331.422° NNW | 2025-12-16 18:36:39.718Z | 278.209° WNW | 24.47° | 2025-12-16 18:38:39.718Z | 236.18° WSW |
| 5 mins | 2025-12-17 05:09:39.718Z | 170.697° S | 2025-12-17 05:11:39.718Z | 193.254° SSW | 43.954° | 2025-12-17 05:14:39.718Z | 345.822° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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