DISKSAT A, 67222
Orbit data source: Space-Track
DISKSAT A, 67222 is a payload satellite owned by USAF STP (US) in LEO that was launched on Thu, 18 Dec 2025 UTC via an ELECTRON launch vehicle from the Wallops Island (WLPIS). 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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67222 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
AERO
Mission
Operational Defense Technology
Bus & Motor
DISKSAT, EP
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl, 1.1 m
Radar Cross Section
0.412 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 DISKSAT A
1 67222U 25305D 26152.11352971 .00010192 00000-0 64364-3 0 9998
2 67222 44.9996 168.5265 0003816 61.5316 298.5944 15.09295949 24881Epoch: 2026-06-01T02:43Z
TLE epoch observation values (Epoch: 2026-06-01T02:43:28.966Z)
Latitude
-0.00004°
Longitude
-121.94975°
Altitude
537.086 km
Speed
7.596 km/s
True Right ascension
11h 14m 06s
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
14:08:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
542.587 km
Perigee altitude
537.307 km
Semi-major axis
6,918.084 km
Eccentricity
0.00038
Inclination
44.9996°
RAAN
168.5265°
Arg. of periapsis
61.5316°
True anomaly
298.556°
Mean anomaly
298.5944°
Eccentric anomaly
298.5752°
Mean motion
3.77194 °/min
Orbital period
95.44 mins
BSTAR
0.00064364
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Other satellites on launch #305 in the year 2025 (2025-12-18 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.DISKSAT A 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-08 05:03:15.244Z | 297.766° NW | 2026-06-08 05:06:15.244Z | 357.788° N | 32.993° | 2026-06-08 05:10:15.244Z | 76.819° E |
| 6 mins | 2026-06-08 06:44:15.244Z | 294.471° NW | 2026-06-08 06:46:15.244Z | 299.725° NW | 42.837° | 2026-06-08 06:50:15.244Z | 113.409° SE |
| 4 mins | 2026-06-08 08:25:15.244Z | 243.006° WSW | 2026-06-08 08:26:15.244Z | 222.77° SW | 19.512° | 2026-06-08 08:29:15.244Z | 172.237° S |
| 6 mins | 2026-06-09 01:33:15.244Z | 229.469° WSW | 2026-06-09 01:36:15.244Z | 132.919° SE | 41.71° | 2026-06-09 01:39:15.244Z | 72.341° E |
| 5 mins | 2026-06-09 03:14:15.244Z | 289.362° WNW | 2026-06-09 03:16:15.244Z | 351.339° N | 35.635° | 2026-06-09 03:19:15.244Z | 59.2° ENE |
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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