FLOCK 4G 5, 62663
Orbit data source: Space-Track
FLOCK 4G 5, 62663 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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62663 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: 20 hours ago
TLE from 20 hours ago
0 FLOCK 4G 5
1 62663U 25009BG 26067.80180090 .00014657 00000-0 52799-3 0 9994
2 62663 97.4059 150.5965 0002122 318.2476 41.8601 15.28666004 63599Epoch: 2026-03-08T19:14Z
TLE epoch observation values (Epoch: 2026-03-08T19:14:35.597Z)
Latitude
-0.0001°
Longitude
55.44431°
Altitude
481.817 km
Speed
7.625 km/s
True Right ascension
10h 02m 23s
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
19:10:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.208 km
Perigee altitude
475.299 km
Semi-major axis
6,854.89 km
Eccentricity
0.00021
Inclination
97.4059°
RAAN
150.5965°
Arg. of periapsis
318.2476°
True anomaly
41.87633°
Mean anomaly
41.8601°
Eccentric anomaly
41.86821°
Mean motion
3.82422 °/min
Orbital period
94.14 mins
BSTAR
0.00052799
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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 5 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 | 2026-03-09 17:47:59.700Z | 33.345° NE | 2026-03-09 17:50:59.700Z | 95.802° ESE | 28.264° | 2026-03-09 17:53:59.700Z | 161.104° S |
| 4 mins | 2026-03-10 05:56:59.700Z | 211.115° SW | 2026-03-10 05:58:59.700Z | 279.474° WNW | 30.091° | 2026-03-10 06:00:59.700Z | 323.796° NNW |
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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