FLOCK 4G 8, 62613
Orbit data source: Space-Track
FLOCK 4G 8, 62613 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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62613 intel report (Beta)
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Edit Public Description
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: 22 hours ago
TLE from 22 hours ago
0 FLOCK 4G 8
1 62613U 25009E 25286.20061900 .00018908 00000-0 80053-3 0 9990
2 62613 97.4229 5.0508 0006102 106.2467 253.9442 15.23203516 41233Epoch: 2025-10-13T04:48Z
TLE epoch observation values (Epoch: 2025-10-13T04:48:53.481Z)
Latitude
0.00002°
Longitude
-89.17885°
Altitude
500.442 km
Speed
7.614 km/s
True Right ascension
00h 20m 12s
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
21:24:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.34 km
Perigee altitude
488.955 km
Semi-major axis
6,871.285 km
Eccentricity
0.00061
Inclination
97.4229°
RAAN
5.0508°
Arg. of periapsis
106.2467°
True anomaly
253.87702°
Mean anomaly
253.9442°
Eccentric anomaly
253.91061°
Mean motion
3.81054 °/min
Orbital period
94.47 mins
BSTAR
0.00080053
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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 8 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 | 2025-10-14 04:37:21.379Z | 106.249° ESE | 2025-10-14 04:39:21.379Z | 63.364° ENE | 19.356° | 2025-10-14 04:41:21.379Z | 25.68° NE |
| 4 mins | 2025-10-14 06:11:21.379Z | 234.263° WSW | 2025-10-14 06:12:21.379Z | 257.061° W | 20.517° | 2025-10-14 06:15:21.379Z | 315.763° NNW |
| 4 mins | 2025-10-14 17:40:21.379Z | 62.789° ENE | 2025-10-14 17:41:21.379Z | 90.453° ESE | 25.293° | 2025-10-14 17:44:21.379Z | 154.95° 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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