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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4G 15
1 62678U 25009BX 26262.19952655 .00007761 00000-0 26044-3 0 9995
2 62678 97.3958 343.7297 0004166 1.9589 358.1668 15.31145800150928Epoch: 2026-09-19T04:47Z
TLE epoch observation values (Epoch: 2026-09-19T04:47:19.093Z)
Latitude
-0.00003°
Longitude
-86.21134°
Altitude
472.645 km
Speed
7.631 km/s
True Right ascension
22h 54m 55s
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
06:37:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.196 km
Perigee altitude
466.49 km
Semi-major axis
6,847.48 km
Eccentricity
0.00042
Inclination
97.3958°
RAAN
343.7297°
Arg. of periapsis
1.9589°
True anomaly
358.16527°
Mean anomaly
358.1668°
Eccentric anomaly
358.16604°
Mean motion
3.83043 °/min
Orbital period
93.98 mins
BSTAR
0.00026044
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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 | 2026-09-19 17:53:57.269Z | 33.814° NE | 2026-09-19 17:56:57.269Z | 97.895° ESE | 32.312° | 2026-09-19 17:59:57.269Z | 161.468° S |
| 4 mins | 2026-09-20 06:01:57.269Z | 214.221° SW | 2026-09-20 06:02:57.269Z | 246.6° WSW | 37.307° | 2026-09-20 06:05:57.269Z | 327.295° NNW |
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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