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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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: 2 days ago
TLE from 2 days ago
0 PREFIRE-1
1 59965U 24108A 26171.41751821 .00003743 00000-0 15902-3 0 9992
2 59965 97.5323 326.2364 0010367 223.4198 136.6223 15.23648011113084Epoch: 2026-06-20T10:01Z
TLE epoch observation values (Epoch: 2026-06-20T10:01:13.573Z)
Latitude
-0.00002°
Longitude
-92.70259°
Altitude
503.123 km
Speed
7.61 km/s
True Right ascension
21h 44m 56s
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
21:38:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.937 km
Perigee altitude
484.693 km
Semi-major axis
6,869.952 km
Eccentricity
0.00104
Inclination
97.5323°
RAAN
326.2364°
Arg. of periapsis
223.4198°
True anomaly
136.70381°
Mean anomaly
136.6223°
Eccentric anomaly
136.66306°
Mean motion
3.81165 °/min
Orbital period
94.45 mins
BSTAR
0.00015902
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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 | 2026-06-22 11:00:47.120Z | 210.77° SW | 2026-06-22 11:02:47.120Z | 251.778° W | 24.536° | 2026-06-22 11:05:47.120Z | 318.535° NNW |
| 4 mins | 2026-06-22 22:30:47.120Z | 67.7° E | 2026-06-22 22:31:47.120Z | 91.449° ESE | 20.842° | 2026-06-22 22:34:47.120Z | 148.53° SSE |
| 4 mins | 2026-06-23 00:03:47.120Z | 325.822° NNW | 2026-06-23 00:05:47.120Z | 282.607° WNW | 19.054° | 2026-06-23 00:07:47.120Z | 245.948° WSW |
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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