FLOCK 4G 9, 62622
Orbit data source: Space-Track
FLOCK 4G 9, 62622 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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62622 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: 2 days ago
TLE from 2 days ago
0 FLOCK 4G 9
1 62622U 25009P 26215.73738637 .00008592 00000-0 30920-3 0 9995
2 62622 97.3939 296.3565 0005717 142.8462 217.3174 15.28827302 86123Epoch: 2026-08-03T17:41Z
TLE epoch observation values (Epoch: 2026-08-03T17:41:50.182Z)
Latitude
-0.00007°
Longitude
78.58122°
Altitude
485.539 km
Speed
7.621 km/s
True Right ascension
19h 45m 25s
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
19:52:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.189 km
Perigee altitude
472.352 km
Semi-major axis
6,854.407 km
Eccentricity
0.00057
Inclination
97.3939°
RAAN
296.3565°
Arg. of periapsis
142.8462°
True anomaly
217.27771°
Mean anomaly
217.3174°
Eccentric anomaly
217.29755°
Mean motion
3.82462 °/min
Orbital period
94.13 mins
BSTAR
0.0003092
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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 9 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-05 05:57:26.831Z | 201.291° SSW | 2026-08-05 05:59:26.831Z | 245.374° WSW | 29.204° | 2026-08-05 06:02:26.831Z | 324.433° NNW |
| 4 mins | 2026-08-05 18:58:26.831Z | 320.342° NNW | 2026-08-05 18:59:26.831Z | 292.87° NW | 24.001° | 2026-08-05 19:02:26.831Z | 231.287° WSW |
| 5 mins | 2026-08-06 05:31:26.831Z | 169.82° S | 2026-08-06 05:33:26.831Z | 182.554° SSW | 43.191° | 2026-08-06 05:36:26.831Z | 346.213° 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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