FLOCK 4G 2, 62661
Orbit data source: Space-Track
FLOCK 4G 2, 62661 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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62661 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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4G 2
1 62661U 25009BE 26262.22102354 .00007593 00000-0 25225-3 0 9997
2 62661 97.3950 343.9413 0003687 11.3152 348.8172 15.31482227150914Epoch: 2026-09-19T05:18Z
TLE epoch observation values (Epoch: 2026-09-19T05:18:16.433Z)
Latitude
-0.00001°
Longitude
-93.75984°
Altitude
472.017 km
Speed
7.631 km/s
True Right ascension
22h 55m 45s
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
05:49:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.864 km
Perigee altitude
465.815 km
Semi-major axis
6,846.476 km
Eccentricity
0.00037
Inclination
97.395°
RAAN
343.9413°
Arg. of periapsis
11.3152°
True anomaly
348.809°
Mean anomaly
348.8172°
Eccentric anomaly
348.8131°
Mean motion
3.83127 °/min
Orbital period
93.96 mins
BSTAR
0.00025225
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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 2 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 | 2026-09-19 18:24:40.705Z | 12.861° NNE | 2026-09-19 18:27:40.705Z | 178.416° S | 78.161° | 2026-09-19 18:30:40.705Z | 191.84° SSW |
| 4 mins | 2026-09-20 04:58:40.705Z | 116.831° SE | 2026-09-20 05:00:40.705Z | 67.867° E | 26.112° | 2026-09-20 05:02:40.705Z | 22.67° NE |
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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