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, 0.8 m
Radar Cross Section
0.930 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 SPIP
1 58298U 23174AU 25291.30888791 .00008049 00000-0 32791-3 0 9998
2 58298 97.4109 5.2660 0008869 327.4278 32.6412 15.24703705107883Epoch: 2025-10-18T07:24Z
TLE epoch observation values (Epoch: 2025-10-18T07:24:47.915Z)
Latitude
0.00003°
Longitude
-132.97541°
Altitude
489.642 km
Speed
7.623 km/s
True Right ascension
00h 21m 03s
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
18:31:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.725 km
Perigee altitude
482.545 km
Semi-major axis
6,866.772 km
Eccentricity
0.00089
Inclination
97.4109°
RAAN
5.266°
Arg. of periapsis
327.4278°
True anomaly
32.69607°
Mean anomaly
32.6412°
Eccentric anomaly
32.66863°
Mean motion
3.81429 °/min
Orbital period
94.38 mins
BSTAR
0.00032791
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-19 05:35:58.161Z | 205.786° SW | 2025-10-19 05:37:58.161Z | 255.495° W | 29.134° | 2025-10-19 05:40:58.161Z | 325.432° NNW |
| 4 mins | 2025-10-19 17:04:58.161Z | 64.623° ENE | 2025-10-19 17:05:58.161Z | 84.233° E | 17.277° | 2025-10-19 17:08:58.161Z | 139.531° SSE |
| 4 mins | 2025-10-19 18:38:58.161Z | 315.612° NNW | 2025-10-19 18:39:58.161Z | 289.297° WNW | 22.951° | 2025-10-19 18:42:58.161Z | 233.182° WSW |
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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