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, 1.0 m
Radar Cross Section
0.338 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 FIREFLY-2
1 62704U 25009CZ 26287.52309440 .00000921 00000-0 94642-4 0 9998
2 62704 97.6931 2.8301 0007605 50.9039 309.2855 14.92690857 95124Epoch: 2026-10-14T12:33Z
TLE epoch observation values (Epoch: 2026-10-14T12:33:15.356Z)
Latitude
-0.00008°
Longitude
151.44453°
Altitude
589.241 km
Speed
7.567 km/s
True Right ascension
00h 11m 19s
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
03:26:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.861 km
Perigee altitude
581.267 km
Semi-major axis
6,964.701 km
Eccentricity
0.00076
Inclination
97.6931°
RAAN
2.8301°
Arg. of periapsis
50.9039°
True anomaly
309.21801°
Mean anomaly
309.2855°
Eccentric anomaly
309.25176°
Mean motion
3.73413 °/min
Orbital period
96.41 mins
BSTAR
0.000094642
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-15 18:04:31.075Z | 10.497° NNE | 2026-10-15 18:08:31.075Z | 214.953° SW | 73.098° | 2026-10-15 18:11:31.075Z | 196.273° SSW |
| 7 mins | 2026-10-16 04:54:31.075Z | 148.889° SSE | 2026-10-16 04:57:31.075Z | 69.795° E | 57.333° | 2026-10-16 05:01:31.075Z | 356.192° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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