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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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, 1.0 m
Radar Cross Section
0.072 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 FLOCK 4G 34
1 62650U 25009AT 25286.17568374 .00017400 00000-0 73995-3 0 9997
2 62650 97.4182 4.9139 0003321 104.4278 255.7328 15.23081754 41231Epoch: 2025-10-13T04:12Z
TLE epoch observation values (Epoch: 2025-10-13T04:12:59.075Z)
Latitude
0.00005°
Longitude
-80.31448°
Altitude
500.209 km
Speed
7.614 km/s
True Right ascension
00h 19m 39s
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
21:23:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.796 km
Perigee altitude
491.232 km
Semi-major axis
6,871.651 km
Eccentricity
0.00033
Inclination
97.4182°
RAAN
4.9139°
Arg. of periapsis
104.4278°
True anomaly
255.69592°
Mean anomaly
255.7328°
Eccentric anomaly
255.71436°
Mean motion
3.81023 °/min
Orbital period
94.48 mins
BSTAR
0.00073995
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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 | 2025-10-14 05:34:15.893Z | 178.204° S | 2025-10-14 05:37:15.893Z | 275.687° WNW | 42.084° | 2025-10-14 05:40:15.893Z | 340.918° N |
| 5 mins | 2025-10-14 18:38:15.893Z | 341.175° N | 2025-10-14 18:40:15.893Z | 265.878° W | 33.27° | 2025-10-14 18:43:15.893Z | 214.317° 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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