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
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: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4G 5
1 62663U 25009BG 26126.49583963 .00008181 00000-0 28615-3 0 9996
2 62663 97.4020 209.0262 0004883 98.1879 261.9915 15.29780474 72563Epoch: 2026-05-06T11:54Z
TLE epoch observation values (Epoch: 2026-05-06T11:54:00.544Z)
Latitude
-0.00004°
Longitude
166.16843°
Altitude
480.04 km
Speed
7.625 km/s
True Right ascension
13h 56m 06s
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
06:55:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.766 km
Perigee altitude
470.075 km
Semi-major axis
6,851.558 km
Eccentricity
0.00049
Inclination
97.402°
RAAN
209.0262°
Arg. of periapsis
98.1879°
True anomaly
261.9361°
Mean anomaly
261.9915°
Eccentric anomaly
261.9638°
Mean motion
3.82701 °/min
Orbital period
94.07 mins
BSTAR
0.00028615
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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 | 2026-05-07 05:17:39.775Z | 153.197° SSE | 2026-05-07 05:20:39.775Z | 86.155° E | 39.831° | 2026-05-07 05:23:39.775Z | 358.61° N |
| 4 mins | 2026-05-07 18:18:39.775Z | 18.856° NNE | 2026-05-07 18:20:39.775Z | 170.451° S | 41.619° | 2026-05-07 18:22:39.775Z | 187.829° SSW |
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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