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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 8
1 62613U 25009E 25338.52883737 .00024931 00000-0 10021-2 0 9993
2 62613 97.4202 56.8422 0003291 284.0369 76.0503 15.24909369 49202Epoch: 2025-12-04T12:41Z
TLE epoch observation values (Epoch: 2025-12-04T12:41:31.548Z)
Latitude
-0.00002°
Longitude
152.87677°
Altitude
493.61 km
Speed
7.618 km/s
True Right ascension
03h 47m 22s
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
10:56:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.277 km
Perigee altitude
485.758 km
Semi-major axis
6,866.154 km
Eccentricity
0.00033
Inclination
97.4202°
RAAN
56.8422°
Arg. of periapsis
284.0369°
True anomaly
76.0869°
Mean anomaly
76.0503°
Eccentric anomaly
76.0686°
Mean motion
3.81481 °/min
Orbital period
94.37 mins
BSTAR
0.0010021
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-05 17:37:01.380Z | 45.949° ENE | 2025-12-05 17:39:01.380Z | 87.438° E | 23.412° | 2025-12-05 17:42:01.380Z | 151.233° SSE |
| 5 mins | 2025-12-06 05:47:01.380Z | 202.144° SSW | 2025-12-06 05:49:01.380Z | 282.782° WNW | 34.788° | 2025-12-06 05:52:01.380Z | 335.244° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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