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: 13 hours ago
TLE from 13 hours ago
0 FLOCK 4G 34
1 62650U 25009AT 26121.98100045 .00011480 00000-0 41821-3 0 9997
2 62650 97.3969 203.8631 0003463 110.7380 249.4231 15.28350510 71859Epoch: 2026-05-01T23:32Z
TLE epoch observation values (Epoch: 2026-05-01T23:32:38.438Z)
Latitude
-0.00005°
Longitude
-9.20252°
Altitude
484.681 km
Speed
7.622 km/s
True Right ascension
13h 35m 27s
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
19:53:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.071 km
Perigee altitude
475.323 km
Semi-major axis
6,855.834 km
Eccentricity
0.00035
Inclination
97.3969°
RAAN
203.8631°
Arg. of periapsis
110.738°
True anomaly
249.38595°
Mean anomaly
249.4231°
Eccentric anomaly
249.40453°
Mean motion
3.82343 °/min
Orbital period
94.16 mins
BSTAR
0.00041821
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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 | 2026-05-02 17:24:24.834Z | 53.894° ENE | 2026-05-02 17:26:24.834Z | 89.096° E | 15.749° | 2026-05-02 17:28:24.834Z | 127.549° SE |
| 4 mins | 2026-05-02 18:58:24.834Z | 328.981° NNW | 2026-05-02 19:00:24.834Z | 276.372° WNW | 23.256° | 2026-05-02 19:02:24.834Z | 236.613° WSW |
| 5 mins | 2026-05-03 05:32:24.834Z | 171.808° S | 2026-05-03 05:34:24.834Z | 249.141° W | 44.713° | 2026-05-03 05:37:24.834Z | 345.743° 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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