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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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: 6 hours ago
TLE from 6 hours ago
0 SPIP
1 58298U 23174AU 26126.94646168 .00004124 00000-0 15681-3 0 9995
2 58298 97.3843 203.8600 0008490 341.6984 18.3949 15.27309634138481Epoch: 2026-05-06T22:42Z
TLE epoch observation values (Epoch: 2026-05-06T22:42:54.289Z)
Latitude
0.00006°
Longitude
-1.66587°
Altitude
481.431 km
Speed
7.628 km/s
True Right ascension
13h 35m 26s
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
13:07:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.637 km
Perigee altitude
474.991 km
Semi-major axis
6,858.951 km
Eccentricity
0.00085
Inclination
97.3843°
RAAN
203.86°
Arg. of periapsis
341.6984°
True anomaly
18.42563°
Mean anomaly
18.3949°
Eccentric anomaly
18.41026°
Mean motion
3.82082 °/min
Orbital period
94.22 mins
BSTAR
0.00015681
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-07 05:07:41.562Z | 165.973° S | 2026-05-07 05:10:41.562Z | 143.666° SSE | 44.778° | 2026-05-07 05:13:41.562Z | 348.906° N |
| 5 mins | 2026-05-07 18:09:41.562Z | 358.668° N | 2026-05-07 18:11:41.562Z | 261.506° W | 41.807° | 2026-05-07 18:14:41.562Z | 203.017° SW |
| 4 mins | 2026-05-08 04:44:41.562Z | 125.2° SE | 2026-05-08 04:46:41.562Z | 55.047° ENE | 30.983° | 2026-05-08 04:48:41.562Z | 10.886° NNE |
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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