PREFIRE-1, 59965
Orbit data source: Space-Track
PREFIRE-1, 59965 is a payload satellite owned by JPL (US) in SSO that was launched on Wed, 05 Jun 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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59965 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: 6 hours ago
TLE from 6 hours ago
0 PREFIRE-1
1 59965U 24108A 25289.57651272 .00007533 00000-0 34874-3 0 9997
2 59965 97.5054 79.4615 0012434 18.6128 341.5560 15.20341468 75536Epoch: 2025-10-16T13:50Z
TLE epoch observation values (Epoch: 2025-10-16T13:50:10.699Z)
Latitude
0.00008°
Longitude
-153.41734°
Altitude
499.778 km
Speed
7.619 km/s
True Right ascension
05h 17m 50s
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
14:33:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.334 km
Perigee altitude
493.225 km
Semi-major axis
6,879.916 km
Eccentricity
0.00124
Inclination
97.5054°
RAAN
79.4615°
Arg. of periapsis
18.6128°
True anomaly
341.51085°
Mean anomaly
341.556°
Eccentric anomaly
341.53343°
Mean motion
3.80337 °/min
Orbital period
94.65 mins
BSTAR
0.00034874
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Other satellites on launch #108 in the year 2024 (2024-06-05 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-1 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 | 2025-10-16 22:18:41.843Z | 46.125° ENE | 2025-10-16 22:20:41.843Z | 85.197° E | 22.802° | 2025-10-16 22:23:41.843Z | 148.588° SSE |
| 5 mins | 2025-10-17 10:30:41.843Z | 198.512° SSW | 2025-10-17 10:32:41.843Z | 265.08° W | 35.401° | 2025-10-17 10:35:41.843Z | 332.894° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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