FLOCK 4G 28, 62634
Orbit data source: Space-Track
FLOCK 4G 28, 62634 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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62634 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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4G 28
1 62634U 25009AB 25309.18803431 .00009831 00000-0 34022-3 0 9999
2 62634 97.4222 28.4248 0002773 53.5068 306.6428 15.30079327 44771Epoch: 2025-11-05T04:30Z
TLE epoch observation values (Epoch: 2025-11-05T04:30:46.164Z)
Latitude
0.00001°
Longitude
-83.93185°
Altitude
477.545 km
Speed
7.628 km/s
True Right ascension
01h 53m 41s
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
07:50:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.428 km
Perigee altitude
470.629 km
Semi-major axis
6,850.666 km
Eccentricity
0.00028
Inclination
97.4222°
RAAN
28.4248°
Arg. of periapsis
53.5068°
True anomaly
306.6173°
Mean anomaly
306.6428°
Eccentric anomaly
306.63005°
Mean motion
3.82775 °/min
Orbital period
94.05 mins
BSTAR
0.00034022
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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 28 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 | 2025-11-05 17:38:40.657Z | 46.17° ENE | 2025-11-05 17:40:40.657Z | 87.718° E | 22.593° | 2025-11-05 17:43:40.657Z | 151.117° SSE |
| 5 mins | 2025-11-06 05:45:40.657Z | 190.911° SSW | 2025-11-06 05:47:40.657Z | 247.032° WSW | 37.03° | 2025-11-06 05:50:40.657Z | 333.992° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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