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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4G 16
1 62638U 25009AF 25357.17243071 .00044869 00000-0 11657-2 0 9991
2 62638 97.4062 77.7661 0001478 192.5576 167.5633 15.38816227 52230Epoch: 2025-12-23T04:08Z
TLE epoch observation values (Epoch: 2025-12-23T04:08:18.013Z)
Latitude
0.00001°
Longitude
-76.26894°
Altitude
453.71 km
Speed
7.64 km/s
True Right ascension
05h 11m 03s
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
11:40:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.558 km
Perigee altitude
445.541 km
Semi-major axis
6,824.686 km
Eccentricity
0.00015
Inclination
97.4062°
RAAN
77.7661°
Arg. of periapsis
192.5576°
True anomaly
167.56695°
Mean anomaly
167.5633°
Eccentric anomaly
167.56512°
Mean motion
3.84963 °/min
Orbital period
93.52 mins
BSTAR
0.0011657
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-23 18:44:39.639Z | 355.219° N | 2025-12-23 18:46:39.639Z | 312.602° NW | 34.3° | 2025-12-23 18:49:39.639Z | 214.969° SW |
| 4 mins | 2025-12-24 05:15:39.639Z | 129.797° SE | 2025-12-24 05:17:39.639Z | 50.653° ENE | 32.257° | 2025-12-24 05:19:39.639Z | 7.4° NNE |
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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