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: 5 hours ago
TLE from 5 hours ago
0 FIREFLY-2
1 62704U 25009CZ 26126.57877808 .00001540 00000-0 15457-3 0 9997
2 62704 97.7029 205.3789 0005334 204.3260 155.7709 14.92720377 71117Epoch: 2026-05-06T13:53Z
TLE epoch observation values (Epoch: 2026-05-06T13:53:26.426Z)
Latitude
0.00006°
Longitude
132.58153°
Altitude
595.892 km
Speed
7.56 km/s
True Right ascension
13h 41m 30s
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
03:08:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.188 km
Perigee altitude
582.758 km
Semi-major axis
6,964.61 km
Eccentricity
0.00053
Inclination
97.7029°
RAAN
205.3789°
Arg. of periapsis
204.326°
True anomaly
155.79597°
Mean anomaly
155.7709°
Eccentric anomaly
155.78344°
Mean motion
3.7342 °/min
Orbital period
96.41 mins
BSTAR
0.00015457
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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 | 2026-05-06 19:17:17.098Z | 325.658° NNW | 2026-05-06 19:19:17.098Z | 294.99° NW | 14.664° | 2026-05-06 19:21:17.098Z | 263.977° W |
| 5 mins | 2026-05-07 04:31:17.098Z | 116.819° SE | 2026-05-07 04:33:17.098Z | 79.09° E | 24.339° | 2026-05-07 04:36:17.098Z | 19.66° NNE |
| 5 mins | 2026-05-07 06:07:17.098Z | 229.382° WSW | 2026-05-07 06:09:17.098Z | 268.972° W | 21.156° | 2026-05-07 06:12:17.098Z | 316.867° NNW |
| 6 mins | 2026-05-07 17:49:17.098Z | 27.821° NE | 2026-05-07 17:52:17.098Z | 115.643° SE | 38.612° | 2026-05-07 17:55:17.098Z | 175.106° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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