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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4G 9
1 62622U 25009P 26171.48156735 .00007254 00000-0 26741-3 0 9991
2 62622 97.3958 252.4065 0003340 325.6146 34.4877 15.28102996 79363Epoch: 2026-06-20T11:33Z
TLE epoch observation values (Epoch: 2026-06-20T11:33:27.419Z)
Latitude
0.00001°
Longitude
170.34669°
Altitude
482.696 km
Speed
7.625 km/s
True Right ascension
16h 49m 37s
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
07:21:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.728 km
Perigee altitude
476.148 km
Semi-major axis
6,856.575 km
Eccentricity
0.00033
Inclination
97.3958°
RAAN
252.4065°
Arg. of periapsis
325.6146°
True anomaly
34.50938°
Mean anomaly
34.4877°
Eccentric anomaly
34.49854°
Mean motion
3.82281 °/min
Orbital period
94.17 mins
BSTAR
0.00026741
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 04:58:36.051Z | 137.706° SSE | 2026-06-21 05:01:36.051Z | 72.621° E | 29.757° | 2026-06-21 05:04:36.051Z | 8.057° NNE |
| 5 mins | 2026-06-21 17:59:36.051Z | 31.631° NE | 2026-06-21 18:01:36.051Z | 87.71° E | 36.504° | 2026-06-21 18:04:36.051Z | 172.211° S |
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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