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: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4G 15
1 62678U 25009BX 26079.65841969 .00010499 00000-0 39263-3 0 9996
2 62678 97.4045 162.0553 0003542 262.8282 97.2554 15.27510969123021Epoch: 2026-03-20T15:48Z
TLE epoch observation values (Epoch: 2026-03-20T15:48:07.461Z)
Latitude
-0.00006°
Longitude
106.8339°
Altitude
486.664 km
Speed
7.622 km/s
True Right ascension
10h 48m 13s
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
07:51:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.641 km
Perigee altitude
477.782 km
Semi-major axis
6,858.349 km
Eccentricity
0.00035
Inclination
97.4045°
RAAN
162.0553°
Arg. of periapsis
262.8282°
True anomaly
97.29566°
Mean anomaly
97.2554°
Eccentric anomaly
97.27553°
Mean motion
3.82132 °/min
Orbital period
94.21 mins
BSTAR
0.00039263
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-21 04:32:20.566Z | 101.81° ESE | 2026-03-21 04:34:20.566Z | 64.227° ENE | 15.686° | 2026-03-21 04:36:20.566Z | 29.417° NE |
| 5 mins | 2026-03-21 06:05:20.566Z | 214.837° SW | 2026-03-21 06:07:20.566Z | 263.453° W | 25.016° | 2026-03-21 06:10:20.566Z | 323.162° NNW |
| 4 mins | 2026-03-21 19:06:20.566Z | 320.711° NNW | 2026-03-21 19:07:20.566Z | 298.56° NW | 19.717° | 2026-03-21 19:10:20.566Z | 240.307° WSW |
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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