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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4G 15
1 62678U 25009BX 26307.47606803 .00008042 00000-0 26238-3 0 9995
2 62678 97.3932 28.8948 0005083 164.0645 196.0757 15.32038284157852Epoch: 2026-11-03T11:25Z
TLE epoch observation values (Epoch: 2026-11-03T11:25:32.277Z)
Latitude
-0.0001°
Longitude
174.77214°
Altitude
476.184 km
Speed
7.626 km/s
True Right ascension
01h 55m 34s
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
14:46:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.16 km
Perigee altitude
463.202 km
Semi-major axis
6,844.818 km
Eccentricity
0.00051
Inclination
97.3932°
RAAN
28.8948°
Arg. of periapsis
164.0645°
True anomaly
196.05958°
Mean anomaly
196.0757°
Eccentric anomaly
196.06764°
Mean motion
3.83266 °/min
Orbital period
93.93 mins
BSTAR
0.00026238
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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 | 2026-11-04 04:49:33.044Z | 106.171° ESE | 2026-11-04 04:51:33.044Z | 63.537° ENE | 19.561° | 2026-11-04 04:53:33.044Z | 25.918° NE |
| 4 mins | 2026-11-04 06:22:33.044Z | 225.118° WSW | 2026-11-04 06:24:33.044Z | 270.773° WNW | 21.806° | 2026-11-04 06:26:33.044Z | 310.823° NW |
| 4 mins | 2026-11-04 17:47:33.044Z | 53.79° ENE | 2026-11-04 17:49:33.044Z | 101.809° ESE | 23.75° | 2026-11-04 17:51:33.044Z | 144.23° SSE |
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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