FLOCK 4BE 26, 60484
Orbit data source: Space-Track
FLOCK 4BE 26, 60484 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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60484 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 5 hours ago
TLE from 5 hours ago
0 FLOCK 4BE 26
1 60484U 24149S 26132.21151088 .00092251 00000-0 11353-2 0 9996
2 60484 97.3671 216.6720 0001518 248.7021 111.4074 15.59934586 96840Epoch: 2026-05-12T05:04Z
TLE epoch observation values (Epoch: 2026-05-12T05:04:34.540Z)
Latitude
0.00002°
Longitude
-89.46106°
Altitude
391.367 km
Speed
7.675 km/s
True Right ascension
14h 26m 41s
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
18:20:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
385.784 km
Perigee altitude
383.731 km
Semi-major axis
6,762.894 km
Eccentricity
0.00015
Inclination
97.3671°
RAAN
216.672°
Arg. of periapsis
248.7021°
True anomaly
111.42359°
Mean anomaly
111.4074°
Eccentric anomaly
111.4155°
Mean motion
3.90251 °/min
Orbital period
92.25 mins
BSTAR
0.0011353
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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 26 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 | 2026-05-12 17:57:47.635Z | 47.539° ENE | 2026-05-12 17:59:47.635Z | 103.429° ESE | 23.264° | 2026-05-12 18:01:47.635Z | 151.806° SSE |
| 4 mins | 2026-05-13 05:50:47.635Z | 183.359° SSW | 2026-05-13 05:52:47.635Z | 274.24° WNW | 40.573° | 2026-05-13 05:54:47.635Z | 336.855° NNW |
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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