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: 5 hours ago
TLE from 5 hours ago
0 SPIP
1 58298U 23174AU 26298.72195233 .00003178 00000-0 11675-3 0 9990
2 58298 97.3744 13.9863 0010725 86.0441 274.2025 15.28608523164717Epoch: 2026-10-25T17:19Z
TLE epoch observation values (Epoch: 2026-10-25T17:19:36.681Z)
Latitude
0.00001°
Longitude
79.97374°
Altitude
482.543 km
Speed
7.624 km/s
True Right ascension
00h 55m 56s
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
17:07:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.276 km
Perigee altitude
469.572 km
Semi-major axis
6,855.061 km
Eccentricity
0.00107
Inclination
97.3744°
RAAN
13.9863°
Arg. of periapsis
86.0441°
True anomaly
274.07992°
Mean anomaly
274.2025°
Eccentric anomaly
274.14121°
Mean motion
3.82407 °/min
Orbital period
94.14 mins
BSTAR
0.00011675
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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 | 2026-10-26 04:28:17.276Z | 116.987° SE | 2026-10-26 04:30:17.276Z | 77.772° E | 22.027° | 2026-10-26 04:33:17.276Z | 18.736° NNE |
| 4 mins | 2026-10-26 06:02:17.276Z | 231.969° WSW | 2026-10-26 06:04:17.276Z | 275.659° WNW | 19.024° | 2026-10-26 06:06:17.276Z | 311.237° NW |
| 5 mins | 2026-10-26 17:28:17.276Z | 45.781° ENE | 2026-10-26 17:30:17.276Z | 94.293° ESE | 29.127° | 2026-10-26 17:33:17.276Z | 157.538° S |
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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