FLOCK 4BE 7, 60481
Orbit data source: Space-Track
FLOCK 4BE 7, 60481 is a payload satellite owned by Planet (US) in SSO that was launched on Fri, 16 Aug 2024 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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60481 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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4BE 7
1 60481U 24149P 26174.64916389 .00017729 00000-0 43811-3 0 9991
2 60481 97.3756 257.7737 0002693 208.6593 151.4506 15.40540692103247Epoch: 2026-06-23T15:34Z
TLE epoch observation values (Epoch: 2026-06-23T15:34:47.760Z)
Latitude
0.00003°
Longitude
112.257°
Altitude
449.246 km
Speed
7.642 km/s
True Right ascension
17h 11m 05s
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
20:00:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.286 km
Perigee altitude
439.613 km
Semi-major axis
6,819.587 km
Eccentricity
0.00027
Inclination
97.3756°
RAAN
257.7737°
Arg. of periapsis
208.6593°
True anomaly
151.46534°
Mean anomaly
151.4506°
Eccentric anomaly
151.45797°
Mean motion
3.85395 °/min
Orbital period
93.41 mins
BSTAR
0.00043811
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Other satellites on launch #149 in the year 2024 (2024-08-16 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 4BE 7 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 | 2026-06-24 18:38:38.945Z | 0.333° NNE | 2026-06-24 18:40:38.945Z | 315.634° NNW | 39.212° | 2026-06-24 18:43:38.945Z | 206.725° SW |
| 4 mins | 2026-06-25 05:08:38.945Z | 124.068° SE | 2026-06-25 05:10:38.945Z | 63.048° ENE | 27.967° | 2026-06-25 05:12:38.945Z | 15.112° NNE |
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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