PREFIRE-2, 59881
Orbit data source: Space-Track
PREFIRE-2, 59881 is a payload satellite owned by JPL (US) in SSO that was launched on Sat, 25 May 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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59881 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
JPL
Mission
Operational Civil Earth Obs Sci
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Sail, 6.3 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 PREFIRE-2
1 59881U 24099A 25287.90126889 .00004930 00000-0 24137-3 0 9998
2 59881 97.4345 143.0903 0012554 351.0217 9.0790 15.18569848 76879Epoch: 2025-10-14T21:37Z
TLE epoch observation values (Epoch: 2025-10-14T21:37:49.632Z)
Latitude
-0.00008°
Longitude
154.95046°
Altitude
504.709 km
Speed
7.617 km/s
True Right ascension
09h 32m 21s
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
02:19:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
515.775 km
Perigee altitude
498.487 km
Semi-major axis
6,885.268 km
Eccentricity
0.00126
Inclination
97.4345°
RAAN
143.0903°
Arg. of periapsis
351.0217°
True anomaly
9.10174°
Mean anomaly
9.079°
Eccentric anomaly
9.09036°
Mean motion
3.79894 °/min
Orbital period
94.76 mins
BSTAR
0.00024137
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Other satellites on launch #99 in the year 2024 (2024-05-25 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.PREFIRE-2 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 | 2025-10-15 13:35:56.494Z | 107.359° ESE | 2025-10-15 13:37:56.494Z | 71.349° E | 17.131° | 2025-10-15 13:39:56.494Z | 33.302° NE |
| 5 mins | 2025-10-15 15:09:56.494Z | 218.798° SW | 2025-10-15 15:11:56.494Z | 267.037° W | 24.296° | 2025-10-15 15:14:56.494Z | 322.687° NNW |
| 5 mins | 2025-10-16 02:40:56.494Z | 51.742° ENE | 2025-10-16 02:42:56.494Z | 97.884° ESE | 23.979° | 2025-10-16 02:45:56.494Z | 153.716° SSE |
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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