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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4G 25
1 62646U 25009AP 25258.49483770 .00010590 00000-0 46019-3 0 9992
2 62646 97.4257 337.7664 0002941 158.8811 201.2548 15.22465471 37025Epoch: 2025-09-15T11:52Z
TLE epoch observation values (Epoch: 2025-09-15T11:52:33.977Z)
Latitude
0.00005°
Longitude
164.92614°
Altitude
503.385 km
Speed
7.612 km/s
True Right ascension
22h 31m 03s
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
15:08:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.392 km
Perigee altitude
493.349 km
Semi-major axis
6,873.507 km
Eccentricity
0.00029
Inclination
97.4257°
RAAN
337.7664°
Arg. of periapsis
158.8811°
True anomaly
201.24259°
Mean anomaly
201.2548°
Eccentric anomaly
201.24869°
Mean motion
3.80869 °/min
Orbital period
94.52 mins
BSTAR
0.00046019
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-16 05:21:25.760Z | 163.048° S | 2025-09-16 05:24:25.760Z | 32.064° NE | 44.29° | 2025-09-16 05:27:25.760Z | 350.551° N |
| 5 mins | 2025-09-16 18:25:25.760Z | 0.065° NNE | 2025-09-16 18:27:25.760Z | 275.972° WNW | 42.405° | 2025-09-16 18:30:25.760Z | 203.132° SW |
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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