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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 FLOCK 4BE 33
1 60502U 24149AL 25258.00560052 .00011052 00000-0 39287-3 0 9994
2 60502 97.3986 335.4470 0005634 172.9958 187.1362 15.29159330 60048Epoch: 2025-09-15T00:08Z
TLE epoch observation values (Epoch: 2025-09-15T00:08:03.884Z)
Latitude
-0.00004°
Longitude
-20.78564°
Altitude
485.261 km
Speed
7.62 km/s
True Right ascension
22h 21m 47s
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
07:39:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.139 km
Perigee altitude
471.416 km
Semi-major axis
6,853.414 km
Eccentricity
0.00056
Inclination
97.3986°
RAAN
335.447°
Arg. of periapsis
172.9958°
True anomaly
187.12819°
Mean anomaly
187.1362°
Eccentric anomaly
187.13219°
Mean motion
3.82545 °/min
Orbital period
94.11 mins
BSTAR
0.00039287
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-15 17:58:37.778Z | 20.286° NNE | 2025-09-15 18:01:37.778Z | 143.723° SSE | 40.666° | 2025-09-15 18:04:37.778Z | 184.191° SSW |
| 4 mins | 2025-09-16 04:33:37.778Z | 108.554° ESE | 2025-09-16 04:35:37.778Z | 62.992° ENE | 20.394° | 2025-09-16 04:37:37.778Z | 23.959° NE |
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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