FIREFLY-1, 62701
Orbit data source: Space-Track
FIREFLY-1, 62701 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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62701 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, 0.9 m
Radar Cross Section
0.338 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 FIREFLY-1
1 62701U 25009CW 26035.24001259 .00002743 00000-0 27105-3 0 9995
2 62701 97.7176 116.0666 0004765 58.2905 301.8778 14.92728933 57488Epoch: 2026-02-04T05:45Z
TLE epoch observation values (Epoch: 2026-02-04T05:45:37.087Z)
Latitude
-0.00008°
Longitude
-104.74736°
Altitude
590.723 km
Speed
7.566 km/s
True Right ascension
07h 44m 15s
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
02:38:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.765 km
Perigee altitude
583.128 km
Semi-major axis
6,964.584 km
Eccentricity
0.00048
Inclination
97.7176°
RAAN
116.0666°
Arg. of periapsis
58.2905°
True anomaly
301.83142°
Mean anomaly
301.8778°
Eccentric anomaly
301.85461°
Mean motion
3.73422 °/min
Orbital period
96.41 mins
BSTAR
0.00027105
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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-1 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-05 04:25:52.993Z | 114.846° SE | 2026-02-05 04:28:52.993Z | 61.681° ENE | 20.691° | 2026-02-05 04:30:52.993Z | 26.593° NE |
| 5 mins | 2026-02-05 06:01:52.993Z | 219.87° SW | 2026-02-05 06:03:52.993Z | 262.367° W | 24.834° | 2026-02-05 06:06:52.993Z | 318.238° NNW |
| 5 mins | 2026-02-05 17:44:52.993Z | 42.281° NE | 2026-02-05 17:46:52.993Z | 100.159° ESE | 34.286° | 2026-02-05 17:49:52.993Z | 165.948° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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