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: 6 hours ago
TLE from 6 hours ago
0 FIREFLY-1
1 62701U 25009CW 25286.55724584 .00003436 00000-0 33713-3 0 9991
2 62701 97.7291 4.4862 0004467 80.9908 279.1817 14.92853982 40529Epoch: 2025-10-13T13:22Z
TLE epoch observation values (Epoch: 2025-10-13T13:22:26.040Z)
Latitude
-0.00001°
Longitude
141.51939°
Altitude
591.59 km
Speed
7.564 km/s
True Right ascension
00h 17m 56s
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
13:49:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.169 km
Perigee altitude
582.947 km
Semi-major axis
6,964.195 km
Eccentricity
0.00045
Inclination
97.7291°
RAAN
4.4862°
Arg. of periapsis
80.9908°
True anomaly
279.13116°
Mean anomaly
279.1817°
Eccentric anomaly
279.15643°
Mean motion
3.73454 °/min
Orbital period
96.4 mins
BSTAR
0.00033713
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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-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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-14 05:35:55.655Z | 187.34° SSW | 2025-10-14 05:37:55.655Z | 236.888° WSW | 39.837° | 2025-10-14 05:41:55.655Z | 338.49° N |
| 4 mins | 2025-10-14 17:19:55.655Z | 71.764° E | 2025-10-14 17:20:55.655Z | 91.673° ESE | 19.648° | 2025-10-14 17:23:55.655Z | 141.613° SSE |
| 5 mins | 2025-10-14 18:54:55.655Z | 328.148° NNW | 2025-10-14 18:56:55.655Z | 279.447° WNW | 25.638° | 2025-10-14 18:59:55.655Z | 230.971° WSW |
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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