FLOCK 4BE 33, 60502
Orbit data source: Space-Track
FLOCK 4BE 33, 60502 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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60502 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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4BE 33
1 60502U 24149AL 25304.17383812 .00074250 00000-0 23831-2 0 9997
2 60502 97.3943 21.4148 0005182 30.3717 329.7824 15.32015518 67107Epoch: 2025-10-31T04:10Z
TLE epoch observation values (Epoch: 2025-10-31T04:10:19.613Z)
Latitude
-0.00003°
Longitude
-80.88898°
Altitude
469.84 km
Speed
7.633 km/s
True Right ascension
01h 25m 39s
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
08:26:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.296 km
Perigee altitude
463.202 km
Semi-major axis
6,844.886 km
Eccentricity
0.00052
Inclination
97.3943°
RAAN
21.4148°
Arg. of periapsis
30.3717°
True anomaly
329.7525°
Mean anomaly
329.7824°
Eccentric anomaly
329.76745°
Mean motion
3.8326 °/min
Orbital period
93.93 mins
BSTAR
0.0023831
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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 33 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 | 2025-10-31 17:17:25.033Z | 54.126° ENE | 2025-10-31 17:19:25.033Z | 90.91° ESE | 16.339° | 2025-10-31 17:21:25.033Z | 130.043° SE |
| 4 mins | 2025-10-31 18:51:25.033Z | 321.87° NNW | 2025-10-31 18:52:25.033Z | 296.681° NW | 22.339° | 2025-10-31 18:55:25.033Z | 234.542° WSW |
| 5 mins | 2025-11-01 05:23:25.033Z | 171.776° S | 2025-11-01 05:25:25.033Z | 211.586° SW | 44.31° | 2025-11-01 05:28:25.033Z | 345.454° 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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