FLOCK 4BE 20, 60489
Orbit data source: Space-Track
FLOCK 4BE 20, 60489 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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60489 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: 14 hours ago
TLE from 14 hours ago
0 FLOCK 4BE 20
1 60489U 24149X 26207.46380079 .00009693 00000-0 25279-3 0 9996
2 60489 97.3687 289.6843 0005575 122.7344 237.4440 15.39028331108259Epoch: 2026-07-26T11:07Z
TLE epoch observation values (Epoch: 2026-07-26T11:07:52.388Z)
Latitude
0.00003°
Longitude
178.55465°
Altitude
454.149 km
Speed
7.639 km/s
True Right ascension
19h 18m 44s
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
14:30:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
449.725 km
Perigee altitude
442.116 km
Semi-major axis
6,824.057 km
Eccentricity
0.00056
Inclination
97.3687°
RAAN
289.6843°
Arg. of periapsis
122.7344°
True anomaly
237.39017°
Mean anomaly
237.444°
Eccentric anomaly
237.41708°
Mean motion
3.85016 °/min
Orbital period
93.5 mins
BSTAR
0.00025279
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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 20 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 | 2026-07-27 05:59:52.156Z | 204.609° SW | 2026-07-27 06:01:52.156Z | 273.345° WNW | 31.515° | 2026-07-27 06:03:52.156Z | 324.442° NNW |
| 4 mins | 2026-07-27 18:54:52.156Z | 332.72° NNW | 2026-07-27 18:55:52.156Z | 304.082° NW | 27.602° | 2026-07-27 18:58:52.156Z | 225.501° WSW |
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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