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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Edit Public Description
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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 FLOCK 4G 16
1 62638U 25009AF 25290.24893225 .00042634 00000-0 13629-2 0 9996
2 62638 97.4137 10.4586 0002206 100.2169 259.9321 15.32312665 41966Epoch: 2025-10-17T05:58Z
TLE epoch observation values (Epoch: 2025-10-17T05:58:27.746Z)
Latitude
-0.00008°
Longitude
-105.15402°
Altitude
472.286 km
Speed
7.63 km/s
True Right ascension
00h 41m 50s
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
16:36:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
467.374 km
Perigee altitude
464.354 km
Semi-major axis
6,844.001 km
Eccentricity
0.00022
Inclination
97.4137°
RAAN
10.4586°
Arg. of periapsis
100.2169°
True anomaly
259.90721°
Mean anomaly
259.9321°
Eccentric anomaly
259.91966°
Mean motion
3.83335 °/min
Orbital period
93.91 mins
BSTAR
0.0013629
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-18 05:36:42.394Z | 174.179° S | 2025-10-18 05:39:42.394Z | 304.404° NW | 42.716° | 2025-10-18 05:42:42.394Z | 344.056° N |
| 5 mins | 2025-10-18 18:35:42.394Z | 353.349° N | 2025-10-18 18:37:42.394Z | 266.55° W | 38.958° | 2025-10-18 18:40:42.394Z | 207.054° 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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