FLOCK 4J 10, 101195
Orbit data source: Space-Track
FLOCK 4J 10, 101195 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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101195 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, 0.2 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4J 10
1 A1195U 26227CY 26302.97178498 .00002430 00000-0 12557-3 0 9993
2 A1195 97.4345 11.9891 0003730 47.7848 312.3702 15.17210323 4300Epoch: 2026-10-29T23:19Z
TLE epoch observation values (Epoch: 2026-10-29T23:19:22.222Z)
Latitude
0.00003°
Longitude
-16.15205°
Altitude
515.63 km
Speed
7.607 km/s
True Right ascension
00h 47m 57s
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
01:40:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.817 km
Perigee altitude
508.677 km
Semi-major axis
6,889.384 km
Eccentricity
0.00037
Inclination
97.4345°
RAAN
11.9891°
Arg. of periapsis
47.7848°
True anomaly
312.33861°
Mean anomaly
312.3702°
Eccentric anomaly
312.35441°
Mean motion
3.79553 °/min
Orbital period
94.85 mins
BSTAR
0.00012557
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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 10 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-30 17:18:00.244Z | 26.054° NE | 2026-10-30 17:21:00.244Z | 96.11° ESE | 49.147° | 2026-10-30 17:24:00.244Z | 172.27° S |
| 4 mins | 2026-10-31 03:59:00.244Z | 94.621° ESE | 2026-10-31 04:00:00.244Z | 72.811° E | 20.785° | 2026-10-31 04:03:00.244Z | 19.715° NNE |
| 5 mins | 2026-10-31 05:32:00.244Z | 220.797° SW | 2026-10-31 05:34:00.244Z | 263.201° W | 23.883° | 2026-10-31 05:37:00.244Z | 318.694° 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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