FLOCK 4J 2, 101072
Orbit data source: Space-Track
FLOCK 4J 2, 101072 is a payload satellite owned by Planet (US) in SSO that was launched on Thu, 01 Oct 2026 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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101072 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Operational spacecraft
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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 FLOCK 4J 2
1 A1072U 26227CB 26308.16945889 .00002645 00000-0 13255-3 0 9994
2 A1072 97.4402 17.1232 0005591 45.5507 314.6183 15.18219616 5067Epoch: 2026-11-04T04:04Z
TLE epoch observation values (Epoch: 2026-11-04T04:04:01.248Z)
Latitude
-0.00006°
Longitude
-87.30362°
Altitude
511.603 km
Speed
7.61 km/s
True Right ascension
01h 08m 29s
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
19:48:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.041 km
Perigee altitude
504.341 km
Semi-major axis
6,886.328 km
Eccentricity
0.00056
Inclination
97.4402°
RAAN
17.1232°
Arg. of periapsis
45.5507°
True anomaly
314.57267°
Mean anomaly
314.6183°
Eccentric anomaly
314.59549°
Mean motion
3.79806 °/min
Orbital period
94.79 mins
BSTAR
0.00013255
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Other satellites on launch #227 in the year 2026 (2026-10-01 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 4J 2 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 | 2026-11-05 03:56:55.228Z | 108.435° ESE | 2026-11-05 03:58:55.228Z | 69.875° E | 20.019° | 2026-11-05 04:00:55.228Z | 30.732° NE |
| 4 mins | 2026-11-05 05:30:55.228Z | 222.57° SW | 2026-11-05 05:32:55.228Z | 268.192° W | 24.496° | 2026-11-05 05:34:55.228Z | 310.086° NW |
| 5 mins | 2026-11-05 17:01:55.228Z | 47.278° ENE | 2026-11-05 17:03:55.228Z | 94.179° ESE | 29.372° | 2026-11-05 17:06:55.228Z | 155.8° SSE |
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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