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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 16
1 62638U 25009AF 25311.19797307 .00048787 00000-0 14679-2 0 9999
2 62638 97.4118 31.4608 0001366 35.6902 324.4432 15.34213151 45175Epoch: 2025-11-07T04:45Z
TLE epoch observation values (Epoch: 2025-11-07T04:45:04.873Z)
Latitude
-0°
Longitude
-86.45489°
Altitude
465.608 km
Speed
7.634 km/s
True Right ascension
02h 05m 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
10:08:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.14 km
Perigee altitude
459.272 km
Semi-major axis
6,838.343 km
Eccentricity
0.00014
Inclination
97.4118°
RAAN
31.4608°
Arg. of periapsis
35.6902°
True anomaly
324.4341°
Mean anomaly
324.4432°
Eccentric anomaly
324.43865°
Mean motion
3.83811 °/min
Orbital period
93.8 mins
BSTAR
0.0014679
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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 | 2025-11-08 18:53:33.417Z | 332.979° NNW | 2025-11-08 18:54:33.417Z | 306.179° NW | 27.123° | 2025-11-08 18:57:33.417Z | 227.765° WSW |
| 4 mins | 2025-11-09 05:25:33.417Z | 150.874° SSE | 2025-11-09 05:26:33.417Z | 123.992° SE | 40.808° | 2025-11-09 05:29:33.417Z | 355.197° N |
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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