FLOCK 4G 25, 62646
Orbit data source: Space-Track
FLOCK 4G 25, 62646 is a payload satellite owned by Planet (US) 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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62646 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5.7 kg wet, 5.7 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.072 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 FLOCK 4G 25
1 62646U 25009AP 25309.47071953 .00011711 00000-0 48556-3 0 9997
2 62646 97.4228 28.1753 0002441 42.0480 318.0945 15.24035832 44789Epoch: 2025-11-05T11:17Z
TLE epoch observation values (Epoch: 2025-11-05T11:17:50.167Z)
Latitude
0.00006°
Longitude
173.77334°
Altitude
495.529 km
Speed
7.618 km/s
True Right ascension
01h 52m 42s
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
03:15:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
492.32 km
Perigee altitude
488.967 km
Semi-major axis
6,868.78 km
Eccentricity
0.00024
Inclination
97.4228°
RAAN
28.1753°
Arg. of periapsis
42.048°
True anomaly
318.07581°
Mean anomaly
318.0945°
Eccentric anomaly
318.08516°
Mean motion
3.81262 °/min
Orbital period
94.42 mins
BSTAR
0.00048556
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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.FLOCK 4G 25 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 | 2025-11-06 17:48:31.712Z | 35.424° NE | 2025-11-06 17:51:31.712Z | 116.228° SE | 30.049° | 2025-11-06 17:53:31.712Z | 159.746° S |
| 4 mins | 2025-11-07 05:59:31.712Z | 223.358° SW | 2025-11-07 06:00:31.712Z | 252.014° W | 27.289° | 2025-11-07 06:03:31.712Z | 322.576° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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