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: 9 hours ago
TLE from 9 hours ago
0 SPIP
1 58298U 23174AU 26234.29801433 .00003941 00000-0 14626-3 0 9995
2 58298 97.3804 310.1844 0007854 320.3834 39.6831 15.28146955154874Epoch: 2026-08-22T07:09Z
TLE epoch observation values (Epoch: 2026-08-22T07:09:08.438Z)
Latitude
0.00001°
Longitude
-127.71119°
Altitude
480.309 km
Speed
7.628 km/s
True Right ascension
20h 40m 44s
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
07:42:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.691 km
Perigee altitude
472.921 km
Semi-major axis
6,856.443 km
Eccentricity
0.00079
Inclination
97.3804°
RAAN
310.1844°
Arg. of periapsis
320.3834°
True anomaly
39.74061°
Mean anomaly
39.6831°
Eccentric anomaly
39.71185°
Mean motion
3.82292 °/min
Orbital period
94.17 mins
BSTAR
0.00014626
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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 | 2026-08-22 17:09:55.847Z | 57.193° ENE | 2026-08-22 17:11:55.847Z | 96.216° ESE | 17.275° | 2026-08-22 17:13:55.847Z | 133.845° SE |
| 4 mins | 2026-08-22 18:43:55.847Z | 321.14° NNW | 2026-08-22 18:44:55.847Z | 296.43° NW | 22.411° | 2026-08-22 18:47:55.847Z | 235.416° WSW |
| 5 mins | 2026-08-23 05:17:55.847Z | 177.242° S | 2026-08-23 05:19:55.847Z | 298.833° NW | 43.297° | 2026-08-23 05:22:55.847Z | 344.126° 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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