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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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: 1 day ago
TLE from 1 day ago
0 FIREFLY-2
1 62704U 25009CZ 26215.93241732 .00000742 00000-0 77201-4 0 9996
2 62704 97.7004 292.8265 0005075 287.2584 72.8080 14.92778232 84445Epoch: 2026-08-03T22:22Z
TLE epoch observation values (Epoch: 2026-08-03T22:22:40.856Z)
Latitude
-0.00001°
Longitude
4.64784°
Altitude
591.279 km
Speed
7.565 km/s
True Right ascension
19h 31m 18s
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
20:02:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.827 km
Perigee altitude
582.758 km
Semi-major axis
6,964.429 km
Eccentricity
0.00051
Inclination
97.7004°
RAAN
292.8265°
Arg. of periapsis
287.2584°
True anomaly
72.86357°
Mean anomaly
72.808°
Eccentric anomaly
72.83578°
Mean motion
3.73435 °/min
Orbital period
96.4 mins
BSTAR
0.000077201
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-05 18:23:48.610Z | 353.189° N | 2026-08-05 18:25:48.610Z | 299.333° NW | 38.695° | 2026-08-05 18:29:48.610Z | 209.797° SW |
| 6 mins | 2026-08-06 05:12:48.610Z | 166.091° S | 2026-08-06 05:14:48.610Z | 164.15° S | 43.102° | 2026-08-06 05:18:48.610Z | 347.985° N |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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