FIREFLY-3, 62710
Orbit data source: Space-Track
FIREFLY-3, 62710 is a payload satellite owned by Pixxel (IN) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62710 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
Pixxel
Mission
Operational Commercial Imaging
Bus & Motor
FIREFLY, Unknown motor
Mass
60 kg wet, 60 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.7 m
Radar Cross Section
0.338 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FIREFLY-3
1 62710U 25009DF 26215.90967744 .00001090 00000-0 11062-3 0 9997
2 62710 97.7037 293.0746 0003552 23.9470 336.1914 14.92844747 84450Epoch: 2026-08-03T21:49Z
TLE epoch observation values (Epoch: 2026-08-03T21:49:56.130Z)
Latitude
-0.00005°
Longitude
13.10472°
Altitude
589.851 km
Speed
7.566 km/s
True Right ascension
19h 32m 17s
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
19:00:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.559 km
Perigee altitude
583.612 km
Semi-major axis
6,964.222 km
Eccentricity
0.00036
Inclination
97.7037°
RAAN
293.0746°
Arg. of periapsis
23.947°
True anomaly
336.17496°
Mean anomaly
336.1914°
Eccentric anomaly
336.18318°
Mean motion
3.73452 °/min
Orbital period
96.4 mins
BSTAR
0.00011062
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.FIREFLY-3 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 | 2026-08-05 06:07:50.645Z | 218.576° SW | 2026-08-05 06:10:50.645Z | 268.814° W | 19.65° | 2026-08-05 06:12:50.645Z | 304.349° NW |
| 6 mins | 2026-08-05 17:50:50.645Z | 25.888° NE | 2026-08-05 17:53:50.645Z | 123.373° SE | 39.93° | 2026-08-05 17:56:50.645Z | 178.237° S |
| 5 mins | 2026-08-06 04:40:50.645Z | 121.65° SE | 2026-08-06 04:42:50.645Z | 71.958° E | 29.983° | 2026-08-06 04:45:50.645Z | 11.062° NNE |
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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