FLOCK 4G 16, 62638
Orbit data source: Space-Track
FLOCK 4G 16, 62638 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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62638 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Non-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: 5 days ago
TLE from 5 days ago
0 FLOCK 4G 16
1 62638U 25009AF 26154.23497242 .00117862 00000-0 13623-2 0 9994
2 62638 97.3855 243.7903 0001696 239.2721 120.8370 15.61488958 77325Epoch: 2026-06-03T05:38Z
TLE epoch observation values (Epoch: 2026-06-03T05:38:21.617Z)
Latitude
0.00003°
Longitude
-92.49628°
Altitude
387.09 km
Speed
7.677 km/s
True Right ascension
16h 15m 09s
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
03:25:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
381.411 km
Perigee altitude
379.119 km
Semi-major axis
6,758.402 km
Eccentricity
0.00017
Inclination
97.3855°
RAAN
243.7903°
Arg. of periapsis
239.2721°
True anomaly
120.85369°
Mean anomaly
120.837°
Eccentric anomaly
120.84534°
Mean motion
3.9064 °/min
Orbital period
92.16 mins
BSTAR
0.0013623
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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 16 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-08 18:25:16.965Z | 42.64° NE | 2026-06-08 18:27:16.965Z | 101.741° ESE | 26.153° | 2026-06-08 18:29:16.965Z | 155.74° SSE |
| 4 mins | 2026-06-09 06:17:16.965Z | 190.696° SSW | 2026-06-09 06:19:16.965Z | 285.931° WNW | 36.545° | 2026-06-09 06:21:16.965Z | 334.522° NNW |
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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