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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 34
1 62650U 25009AT 26305.17434495 .00012248 00000-0 40447-3 0 9997
2 62650 97.3877 26.1584 0002726 148.5765 211.5639 15.31535192 99865Epoch: 2026-11-01T04:11Z
TLE epoch observation values (Epoch: 2026-11-01T04:11:03.403Z)
Latitude
-0.00011°
Longitude
-77.07527°
Altitude
475.929 km
Speed
7.627 km/s
True Right ascension
01h 44m 38s
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
10:36:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.047 km
Perigee altitude
466.315 km
Semi-major axis
6,846.318 km
Eccentricity
0.00027
Inclination
97.3877°
RAAN
26.1584°
Arg. of periapsis
148.5765°
True anomaly
211.54755°
Mean anomaly
211.5639°
Eccentric anomaly
211.55573°
Mean motion
3.8314 °/min
Orbital period
93.96 mins
BSTAR
0.00040447
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-02 18:22:56.955Z | 14.261° NNE | 2026-11-02 18:25:56.955Z | 174.43° S | 68.378° | 2026-11-02 18:28:56.955Z | 190.493° SSW |
| 4 mins | 2026-11-03 04:56:56.955Z | 112.34° ESE | 2026-11-03 04:58:56.955Z | 61.99° ENE | 24.843° | 2026-11-03 05:00:56.955Z | 20.995° NNE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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