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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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 + 2 Pan, 6.3 m
Radar Cross Section
0.789 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 PREFIRE-2
1 59881U 24099A 26252.58383654 .00002618 00000-0 11914-3 0 9990
2 59881 97.3981 107.3723 0010264 271.3222 88.6838 15.21547753126960Epoch: 2026-09-09T14:00Z
TLE epoch observation values (Epoch: 2026-09-09T14:00:43.477Z)
Latitude
-0.00001°
Longitude
-91.44266°
Altitude
504.109 km
Speed
7.612 km/s
True Right ascension
07h 09m 29s
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
07:32:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.193 km
Perigee altitude
491.077 km
Semi-major axis
6,876.272 km
Eccentricity
0.00103
Inclination
97.3981°
RAAN
107.3723°
Arg. of periapsis
271.3222°
True anomaly
88.80139°
Mean anomaly
88.6838°
Eccentric anomaly
88.74259°
Mean motion
3.80639 °/min
Orbital period
94.58 mins
BSTAR
0.00011914
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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 | 2026-09-10 15:24:05.213Z | 229.804° WSW | 2026-09-10 15:26:05.213Z | 266.002° W | 17.231° | 2026-09-10 15:28:05.213Z | 302.354° NW |
| 5 mins | 2026-09-11 02:54:05.213Z | 42.588° NE | 2026-09-11 02:56:05.213Z | 109.246° ESE | 40.688° | 2026-09-11 02:59:05.213Z | 168.815° S |
| 4 mins | 2026-09-11 15:05:05.213Z | 220.993° SW | 2026-09-11 15:07:05.213Z | 275.383° WNW | 28.569° | 2026-09-11 15:09:05.213Z | 316.77° NNW |
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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