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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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: 12 hours ago
TLE from 12 hours ago
0 FLOCK 4G 8
1 62613U 25009E 26095.18126259 .00014890 00000-0 54149-3 0 9998
2 62613 97.4019 177.5687 0004082 194.5554 165.5569 15.28344127 67768Epoch: 2026-04-05T04:21Z
TLE epoch observation values (Epoch: 2026-04-05T04:21:01.087Z)
Latitude
-0.00002°
Longitude
-81.1762°
Altitude
486.576 km
Speed
7.62 km/s
True Right ascension
11h 50m 16s
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
21:59:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.515 km
Perigee altitude
474.918 km
Semi-major axis
6,855.854 km
Eccentricity
0.00041
Inclination
97.4019°
RAAN
177.5687°
Arg. of periapsis
194.5554°
True anomaly
165.56856°
Mean anomaly
165.5569°
Eccentric anomaly
165.56273°
Mean motion
3.82341 °/min
Orbital period
94.16 mins
BSTAR
0.00054149
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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 | 2026-04-05 17:29:47.401Z | 49.7° ENE | 2026-04-05 17:31:47.401Z | 85.357° E | 17.719° | 2026-04-05 17:33:47.401Z | 128.127° SE |
| 4 mins | 2026-04-05 19:03:47.401Z | 328.409° NNW | 2026-04-05 19:05:47.401Z | 281.511° WNW | 20.979° | 2026-04-05 19:07:47.401Z | 242.116° WSW |
| 5 mins | 2026-04-06 05:37:47.401Z | 178.804° S | 2026-04-06 05:39:47.401Z | 237.928° WSW | 42.83° | 2026-04-06 05:42:47.401Z | 341.484° N |
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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