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: 2 days ago
TLE from 2 days ago
0 FLOCK 4G 16
1 62638U 25009AF 25324.49656802 .00039234 00000-0 11283-2 0 9995
2 62638 97.4106 44.8244 0001124 336.8678 23.2515 15.35691713 47212Epoch: 2025-11-20T11:55Z
TLE epoch observation values (Epoch: 2025-11-20T11:55:03.476Z)
Latitude
-0.00003°
Longitude
166.30681°
Altitude
461.272 km
Speed
7.636 km/s
True Right ascension
02h 59m 17s
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
11:33:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.58 km
Perigee altitude
455.044 km
Semi-major axis
6,833.949 km
Eccentricity
0.00011
Inclination
97.4106°
RAAN
44.8244°
Arg. of periapsis
336.8678°
True anomaly
23.25659°
Mean anomaly
23.2515°
Eccentric anomaly
23.25404°
Mean motion
3.84181 °/min
Orbital period
93.71 mins
BSTAR
0.0011283
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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 | 2025-11-22 17:39:55.771Z | 54.397° ENE | 2025-11-22 17:41:55.771Z | 98.962° ESE | 19.799° | 2025-11-22 17:43:55.771Z | 140.458° SSE |
| 5 mins | 2025-11-23 05:43:55.771Z | 181.96° SSW | 2025-11-23 05:45:55.771Z | 251.133° W | 41.823° | 2025-11-23 05:48:55.771Z | 340.287° 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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