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, 0.1 m
Radar Cross Section
0.035 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 28
1 62634U 25009AB 25260.81008762 .00034107 00000-0 13361-2 0 9995
2 62634 97.4262 340.2029 0005547 179.8331 180.2910 15.25697068 37387Epoch: 2025-09-17T19:26Z
TLE epoch observation values (Epoch: 2025-09-17T19:26:31.57Z)
Latitude
-0.00001°
Longitude
51.59066°
Altitude
495.6 km
Speed
7.615 km/s
True Right ascension
22h 40m 48s
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
16:26:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.46 km
Perigee altitude
481.845 km
Semi-major axis
6,863.789 km
Eccentricity
0.00055
Inclination
97.4262°
RAAN
340.2029°
Arg. of periapsis
179.8331°
True anomaly
180.29068°
Mean anomaly
180.291°
Eccentric anomaly
180.29084°
Mean motion
3.81678 °/min
Orbital period
94.32 mins
BSTAR
0.0013361
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-19 04:38:59.396Z | 111.263° ESE | 2025-09-19 04:40:59.396Z | 70.321° E | 19.916° | 2025-09-19 04:42:59.396Z | 28.932° NE |
| 4 mins | 2025-09-19 06:12:59.396Z | 232.44° WSW | 2025-09-19 06:13:59.396Z | 254.057° W | 19.709° | 2025-09-19 06:16:59.396Z | 313.783° NW |
| 4 mins | 2025-09-19 17:40:59.396Z | 62.553° ENE | 2025-09-19 17:41:59.396Z | 90.075° ESE | 24.933° | 2025-09-19 17:44:59.396Z | 154.782° 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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