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: 1 day ago
TLE from 1 day ago
0 PREFIRE-1
1 59965U 24108A 25260.94101808 .00004848 00000-0 22921-3 0 9998
2 59965 97.5021 50.9766 0013537 111.6291 248.6388 15.19784771 71189Epoch: 2025-09-17T22:35Z
TLE epoch observation values (Epoch: 2025-09-17T22:35:03.962Z)
Latitude
0.00008°
Longitude
75.10033°
Altitude
512.984 km
Speed
7.605 km/s
True Right ascension
03h 23m 54s
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
18:53:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.776 km
Perigee altitude
494.145 km
Semi-major axis
6,881.598 km
Eccentricity
0.00135
Inclination
97.5021°
RAAN
50.9766°
Arg. of periapsis
111.6291°
True anomaly
248.49442°
Mean anomaly
248.6388°
Eccentric anomaly
248.5666°
Mean motion
3.80197 °/min
Orbital period
94.69 mins
BSTAR
0.00022921
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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 | 2025-09-19 09:29:12.019Z | 127.314° SE | 2025-09-19 09:32:12.019Z | 65.328° ENE | 24.552° | 2025-09-19 09:34:12.019Z | 21.798° NNE |
| 5 mins | 2025-09-19 22:34:12.019Z | 38.802° NE | 2025-09-19 22:36:12.019Z | 94.491° ESE | 32.649° | 2025-09-19 22:39:12.019Z | 166.331° S |
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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