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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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, 0.7 m
Radar Cross Section
0.338 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 FIREFLY-3
1 62710U 25009DF 25286.24525704 .00003679 00000-0 36084-3 0 9993
2 62710 97.7285 4.2439 0002441 268.4984 91.5956 14.92831788 40493Epoch: 2025-10-13T05:53Z
TLE epoch observation values (Epoch: 2025-10-13T05:53:10.208Z)
Latitude
0.00001°
Longitude
-106.09944°
Altitude
592.203 km
Speed
7.564 km/s
True Right ascension
00h 16m 58s
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
11:32:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.827 km
Perigee altitude
584.427 km
Semi-major axis
6,964.264 km
Eccentricity
0.00024
Inclination
97.7285°
RAAN
4.2439°
Arg. of periapsis
268.4984°
True anomaly
91.62356°
Mean anomaly
91.5956°
Eccentric anomaly
91.60958°
Mean motion
3.73448 °/min
Orbital period
96.4 mins
BSTAR
0.00036084
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-13 17:42:56.366Z | 29.631° NE | 2025-10-13 17:46:56.366Z | 114.942° SE | 32.079° | 2025-10-13 17:49:56.366Z | 166.312° S |
| 5 mins | 2025-10-14 04:33:56.366Z | 110.187° ESE | 2025-10-14 04:35:56.366Z | 69.568° E | 23.317° | 2025-10-14 04:38:56.366Z | 17.214° NNE |
| 4 mins | 2025-10-14 06:09:56.366Z | 233.97° WSW | 2025-10-14 06:10:56.366Z | 254.56° W | 22.015° | 2025-10-14 06:13:56.366Z | 311.734° NW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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