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: 8 hours ago
TLE from 8 hours ago
0 SPIP
1 58298U 23174AU 26248.31044941 .00002427 00000-0 90850-4 0 9998
2 58298 97.3787 324.0634 0007522 260.2714 99.7676 15.28244256157012Epoch: 2026-09-05T07:27Z
TLE epoch observation values (Epoch: 2026-09-05T07:27:02.829Z)
Latitude
-0.00002°
Longitude
-132.12014°
Altitude
485.042 km
Speed
7.622 km/s
True Right ascension
21h 36m 15s
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
07:14:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.172 km
Perigee altitude
472.857 km
Semi-major axis
6,856.151 km
Eccentricity
0.00075
Inclination
97.3787°
RAAN
324.0634°
Arg. of periapsis
260.2714°
True anomaly
99.85253°
Mean anomaly
99.7676°
Eccentric anomaly
99.81007°
Mean motion
3.82316 °/min
Orbital period
94.16 mins
BSTAR
0.00009085
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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 | 2026-09-05 17:26:35.275Z | 35.183° NE | 2026-09-05 17:29:35.275Z | 94.899° ESE | 26.178° | 2026-09-05 17:32:35.275Z | 157.815° S |
| 5 mins | 2026-09-06 05:35:35.275Z | 203.427° SW | 2026-09-06 05:37:35.275Z | 271.695° WNW | 33.261° | 2026-09-06 05:40:35.275Z | 332.396° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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