FLOCK 4G 27, 62641
Orbit data source: Space-Track
FLOCK 4G 27, 62641 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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62641 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 27
1 62641U 25009AJ 26074.45413426 .00011347 00000-0 42620-3 0 9996
2 62641 97.3976 156.5159 0000749 262.2225 97.8929 15.27349209 64584Epoch: 2026-03-15T10:53Z
TLE epoch observation values (Epoch: 2026-03-15T10:53:57.200Z)
Latitude
-0.00001°
Longitude
179.96683°
Altitude
486.911 km
Speed
7.622 km/s
True Right ascension
10h 26m 03s
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
00:36:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.21 km
Perigee altitude
480.182 km
Semi-major axis
6,858.833 km
Eccentricity
0.00007
Inclination
97.3976°
RAAN
156.5159°
Arg. of periapsis
262.2225°
True anomaly
97.9014°
Mean anomaly
97.8929°
Eccentric anomaly
97.89715°
Mean motion
3.82092 °/min
Orbital period
94.22 mins
BSTAR
0.0004262
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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 27 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 | 2026-03-16 05:54:58.463Z | 215.821° SW | 2026-03-16 05:55:58.463Z | 246.473° WSW | 30.251° | 2026-03-16 05:58:58.463Z | 325.647° NNW |
| 4 mins | 2026-03-16 18:54:58.463Z | 334.167° NNW | 2026-03-16 18:56:58.463Z | 284.3° WNW | 24.534° | 2026-03-16 18:58:58.463Z | 239.039° WSW |
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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