FLOCK 4J 1, 101071
Orbit data source: Space-Track
FLOCK 4J 1, 101071 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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101071 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 1
1 A1071U 26227CA 26308.16846785 .00003118 00000-0 15546-3 0 9999
2 A1071 97.4404 17.1253 0005588 41.6103 318.5555 15.18266567 5070Epoch: 2026-11-04T04:02Z
TLE epoch observation values (Epoch: 2026-11-04T04:02:35.622Z)
Latitude
-0.00005°
Longitude
-86.94377°
Altitude
511.281 km
Speed
7.61 km/s
True Right ascension
01h 08m 30s
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
19:48:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.897 km
Perigee altitude
504.201 km
Semi-major axis
6,886.186 km
Eccentricity
0.00056
Inclination
97.4404°
RAAN
17.1253°
Arg. of periapsis
41.6103°
True anomaly
318.51309°
Mean anomaly
318.5555°
Eccentric anomaly
318.5343°
Mean motion
3.79818 °/min
Orbital period
94.78 mins
BSTAR
0.00015546
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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 1 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 | 2026-11-05 03:54:50.551Z | 115.174° SE | 2026-11-05 03:57:50.551Z | 61.403° ENE | 19.078° | 2026-11-05 03:59:50.551Z | 26.395° NE |
| 4 mins | 2026-11-05 05:29:50.551Z | 228.035° WSW | 2026-11-05 05:30:50.551Z | 251.112° W | 24.849° | 2026-11-05 05:33:50.551Z | 315.735° NNW |
| 4 mins | 2026-11-05 17:00:50.551Z | 54.58° ENE | 2026-11-05 17:02:50.551Z | 106.448° ESE | 27.769° | 2026-11-05 17:04:50.551Z | 148.172° 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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