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 spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 PREFIRE-1
1 59965U 24108A 25258.24151809 .00007257 00000-0 34167-3 0 9996
2 59965 97.5024 48.2937 0013429 120.1138 240.1430 15.19759744 70778Epoch: 2025-09-15T05:47Z
TLE epoch observation values (Epoch: 2025-09-15T05:47:47.162Z)
Latitude
-0.00003°
Longitude
-33.1018°
Altitude
514.266 km
Speed
7.604 km/s
True Right ascension
03h 13m 10s
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
10:20:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.778 km
Perigee altitude
494.295 km
Semi-major axis
6,881.673 km
Eccentricity
0.00134
Inclination
97.5024°
RAAN
48.2937°
Arg. of periapsis
120.1138°
True anomaly
240.00965°
Mean anomaly
240.143°
Eccentric anomaly
240.07631°
Mean motion
3.80191 °/min
Orbital period
94.69 mins
BSTAR
0.00034167
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-15 22:10:47.927Z | 52.148° ENE | 2025-09-15 22:12:47.927Z | 90.662° ESE | 19.254° | 2025-09-15 22:14:47.927Z | 132.668° SE |
| 5 mins | 2025-09-16 10:22:47.927Z | 188.156° SSW | 2025-09-16 10:24:47.927Z | 255.713° W | 39.957° | 2025-09-16 10:27:47.927Z | 336.897° 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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