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: 8 hours ago
TLE from 8 hours ago
0 FIREFLY-3
1 62710U 25009DF 25335.24348096 .00002951 00000-0 29115-3 0 9994
2 62710 97.7258 52.3483 0007024 103.3985 256.8018 14.92720581 47801Epoch: 2025-12-01T05:50Z
TLE epoch observation values (Epoch: 2025-12-01T05:50:36.754Z)
Latitude
-0.00002°
Longitude
-105.65061°
Altitude
593.622 km
Speed
7.562 km/s
True Right ascension
03h 29m 23s
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
11:42:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.365 km
Perigee altitude
581.581 km
Semi-major axis
6,964.61 km
Eccentricity
0.0007
Inclination
97.7258°
RAAN
52.3483°
Arg. of periapsis
103.3985°
True anomaly
256.72345°
Mean anomaly
256.8018°
Eccentric anomaly
256.76262°
Mean motion
3.7342 °/min
Orbital period
96.41 mins
BSTAR
0.00029115
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
Did you know?
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 | 2025-12-01 17:40:17.309Z | 29.856° NE | 2025-12-01 17:44:17.309Z | 109.827° ESE | 31.268° | 2025-12-01 17:47:17.309Z | 164.059° S |
| 5 mins | 2025-12-02 04:31:17.309Z | 111.953° ESE | 2025-12-02 04:33:17.309Z | 74.526° E | 22.342° | 2025-12-02 04:36:17.309Z | 20.003° NNE |
| 5 mins | 2025-12-02 06:07:17.309Z | 229.184° WSW | 2025-12-02 06:09:17.309Z | 273.169° WNW | 22.802° | 2025-12-02 06:12:17.309Z | 320.333° NNW |
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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