FLOCK 4G 34, 62650
Orbit data source: Space-Track
FLOCK 4G 34, 62650 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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62650 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4G 34
1 62650U 25009AT 26238.17716070 .00007190 00000-0 24750-3 0 9993
2 62650 97.3941 319.4317 0003390 78.3445 281.8176 15.30350059 89616Epoch: 2026-08-26T04:15Z
TLE epoch observation values (Epoch: 2026-08-26T04:15:06.684Z)
Latitude
-0.00003°
Longitude
-78.78005°
Altitude
477.397 km
Speed
7.627 km/s
True Right ascension
21h 17m 43s
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
04:37:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.041 km
Perigee altitude
469.396 km
Semi-major axis
6,849.856 km
Eccentricity
0.00034
Inclination
97.3941°
RAAN
319.4317°
Arg. of periapsis
78.3445°
True anomaly
281.77957°
Mean anomaly
281.8176°
Eccentric anomaly
281.79859°
Mean motion
3.82843 °/min
Orbital period
94.03 mins
BSTAR
0.0002475
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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 34 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-26 18:57:05.098Z | 330.451° NNW | 2026-08-26 18:58:05.098Z | 304.512° NW | 25.892° | 2026-08-26 19:01:05.098Z | 230.418° WSW |
| 5 mins | 2026-08-27 05:30:05.098Z | 162.021° S | 2026-08-27 05:32:05.098Z | 100.849° ESE | 44.535° | 2026-08-27 05:35:05.098Z | 350.779° N |
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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