FIREFLY-2, 62704
Orbit data source: Space-Track
FIREFLY-2, 62704 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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62704 intel report (Beta)
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Edit Public Description
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, 0.9 m
Radar Cross Section
0.338 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 FIREFLY-2
1 62704U 25009CZ 25338.61698713 .00004680 00000-0 45815-3 0 9991
2 62704 97.7222 55.4906 0006021 21.4412 338.7059 14.92758640 48296Epoch: 2025-12-04T14:48Z
TLE epoch observation values (Epoch: 2025-12-04T14:48:27.688Z)
Latitude
0.00005°
Longitude
119.70436°
Altitude
588.473 km
Speed
7.568 km/s
True Right ascension
03h 41m 57s
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
10:59:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.548 km
Perigee altitude
582.161 km
Semi-major axis
6,964.491 km
Eccentricity
0.0006
Inclination
97.7222°
RAAN
55.4906°
Arg. of periapsis
21.4412°
True anomaly
338.68083°
Mean anomaly
338.7059°
Eccentric anomaly
338.69336°
Mean motion
3.7343 °/min
Orbital period
96.4 mins
BSTAR
0.00045815
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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-2 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 | 2025-12-05 17:08:29.834Z | 57.92° ENE | 2025-12-05 17:10:29.834Z | 89.308° E | 16.083° | 2025-12-05 17:12:29.834Z | 122.698° SE |
| 5 mins | 2025-12-05 18:44:29.834Z | 336.651° NNW | 2025-12-05 18:46:29.834Z | 282.112° WNW | 30.775° | 2025-12-05 18:49:29.834Z | 225.264° WSW |
| 6 mins | 2025-12-06 05:33:29.834Z | 186.605° SSW | 2025-12-06 05:35:29.834Z | 244.217° WSW | 40.915° | 2025-12-06 05:39:29.834Z | 339.679° N |
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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