FLOCK 4BE 12, 60560
Orbit data source: Space-Track
FLOCK 4BE 12, 60560 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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60560 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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4BE 12
1 60560U 24149CW 26084.49717941 .00128672 00000-0 22275-2 0 9995
2 60560 97.3720 168.8013 0007270 219.2404 140.8321 15.50436295 89514Epoch: 2026-03-25T11:55Z
TLE epoch observation values (Epoch: 2026-03-25T11:55:56.301Z)
Latitude
-0.00004°
Longitude
166.85708°
Altitude
422.415 km
Speed
7.656 km/s
True Right ascension
11h 15m 12s
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
23:34:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
417.312 km
Perigee altitude
407.438 km
Semi-major axis
6,790.512 km
Eccentricity
0.00073
Inclination
97.372°
RAAN
168.8013°
Arg. of periapsis
219.2404°
True anomaly
140.88468°
Mean anomaly
140.8321°
Eccentric anomaly
140.85839°
Mean motion
3.87873 °/min
Orbital period
92.81 mins
BSTAR
0.0022275
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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 12 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 | 2026-03-25 18:41:29.076Z | 355.594° N | 2026-03-25 18:43:29.076Z | 291.686° WNW | 37.668° | 2026-03-25 18:46:29.076Z | 208.842° SW |
| 4 mins | 2026-03-26 05:07:29.076Z | 118.458° SE | 2026-03-26 05:08:29.076Z | 91.28° ESE | 25.499° | 2026-03-26 05:11:29.076Z | 12.772° NNE |
| 4 mins | 2026-03-26 17:56:29.076Z | 53.906° ENE | 2026-03-26 17:57:29.076Z | 81.841° E | 24.758° | 2026-03-26 18:00:29.076Z | 157.853° S |
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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