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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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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4G 25
1 62646U 25009AP 26305.14544079 .00011250 00000-0 36779-3 0 9994
2 62646 97.3930 26.7762 0002548 143.8350 216.3064 15.31884065 99876Epoch: 2026-11-01T03:29Z
TLE epoch observation values (Epoch: 2026-11-01T03:29:26.084Z)
Latitude
-0.00004°
Longitude
-66.02349°
Altitude
474.705 km
Speed
7.628 km/s
True Right ascension
01h 47m 06s
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
04:54:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.885 km
Perigee altitude
465.397 km
Semi-major axis
6,845.278 km
Eccentricity
0.00025
Inclination
97.393°
RAAN
26.7762°
Arg. of periapsis
143.835°
True anomaly
216.28912°
Mean anomaly
216.3064°
Eccentric anomaly
216.29776°
Mean motion
3.83227 °/min
Orbital period
93.94 mins
BSTAR
0.00036779
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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 | 2026-11-01 18:10:09.115Z | 28.553° NE | 2026-11-01 18:12:09.115Z | 70.155° E | 44.348° | 2026-11-01 18:15:09.115Z | 170.645° S |
| 4 mins | 2026-11-02 06:17:09.115Z | 224.178° SW | 2026-11-02 06:19:09.115Z | 278.476° WNW | 25.33° | 2026-11-02 06:21:09.115Z | 317.426° NNW |
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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