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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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 5
1 62663U 25009BG 25286.17016319 .00039742 00000-0 16545-2 0 9998
2 62663 97.4240 4.9800 0005097 111.9219 248.2560 15.23618944 41226Epoch: 2025-10-13T04:05Z
TLE epoch observation values (Epoch: 2025-10-13T04:05:02.099Z)
Latitude
-0.00006°
Longitude
-78.25553°
Altitude
499.33 km
Speed
7.614 km/s
True Right ascension
00h 19m 55s
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
21:24:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.399 km
Perigee altitude
488.396 km
Semi-major axis
6,870.034 km
Eccentricity
0.00051
Inclination
97.424°
RAAN
4.98°
Arg. of periapsis
111.9219°
True anomaly
248.20176°
Mean anomaly
248.256°
Eccentric anomaly
248.22888°
Mean motion
3.81158 °/min
Orbital period
94.45 mins
BSTAR
0.0016545
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
Did you know?
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 | 2025-10-14 05:25:20.711Z | 168.154° S | 2025-10-14 05:28:20.711Z | 176.864° S | 43.471° | 2025-10-14 05:31:20.711Z | 346.894° N |
| 5 mins | 2025-10-14 18:29:20.711Z | 354.185° N | 2025-10-14 18:31:20.711Z | 268.704° W | 39.815° | 2025-10-14 18:34:20.711Z | 206.815° 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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