FLOCK 4G 15, 62678
Orbit data source: Space-Track
FLOCK 4G 15, 62678 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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62678 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 15
1 62678U 25009BX 26170.78590084 .00008616 00000-0 30463-3 0 9992
2 62678 97.4016 252.6502 0003385 316.9109 43.1866 15.29417410136943Epoch: 2026-06-19T18:51Z
TLE epoch observation values (Epoch: 2026-06-19T18:51:41.832Z)
Latitude
-0.00002°
Longitude
61.71602°
Altitude
478.964 km
Speed
7.627 km/s
True Right ascension
16h 50m 36s
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
07:24:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.825 km
Perigee altitude
472.186 km
Semi-major axis
6,852.643 km
Eccentricity
0.00034
Inclination
97.4016°
RAAN
252.6502°
Arg. of periapsis
316.9109°
True anomaly
43.21315°
Mean anomaly
43.1866°
Eccentric anomaly
43.19988°
Mean motion
3.8261 °/min
Orbital period
94.09 mins
BSTAR
0.00030463
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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 15 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 | 2026-06-21 05:31:27.900Z | 167.71° S | 2026-06-21 05:34:27.900Z | 172.124° S | 42.627° | 2026-06-21 05:37:27.900Z | 347.31° N |
| 5 mins | 2026-06-21 18:32:27.900Z | 359.745° N | 2026-06-21 18:34:27.900Z | 288.146° WNW | 41.827° | 2026-06-21 18:37:27.900Z | 204.274° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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