BLACKCAT, 67369
Orbit data source: Space-Track
BLACKCAT, 67369 is a payload satellite owned by PSU (US) in SSO that was launched on Sun, 11 Jan 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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67369 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NanoAvionics US
Mission
Operational Amateur Astronomy
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
11.4 kg wet, 11.4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
0.078 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 BLACKCAT
1 67369U 26004G 26264.26207499 .00000564 00000-0 67621-4 0 9993
2 67369 97.8053 261.1291 0006952 176.1274 183.9997 14.87875759 37576Epoch: 2026-09-21T06:17Z
TLE epoch observation values (Epoch: 2026-09-21T06:17:23.279Z)
Latitude
-0.00006°
Longitude
166.63768°
Altitude
612.453 km
Speed
7.55 km/s
True Right ascension
17h 24m 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
13:29:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
606.452 km
Perigee altitude
596.748 km
Semi-major axis
6,979.737 km
Eccentricity
0.0007
Inclination
97.8053°
RAAN
261.1291°
Arg. of periapsis
176.1274°
True anomaly
183.99415°
Mean anomaly
183.9997°
Eccentric anomaly
183.99692°
Mean motion
3.72207 °/min
Orbital period
96.72 mins
BSTAR
0.000067621
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Other satellites on launch #4 in the year 2026 (2026-01-11 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.BLACKCAT 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 | 2026-09-22 00:10:59.915Z | 187.198° SSW | 2026-09-22 00:12:59.915Z | 237.566° WSW | 58.056° | 2026-09-22 00:16:59.915Z | 338.481° N |
| 4 mins | 2026-09-22 11:56:59.915Z | 64.634° ENE | 2026-09-22 11:58:59.915Z | 105.102° ESE | 22.093° | 2026-09-22 12:00:59.915Z | 138.552° SSE |
| 5 mins | 2026-09-22 13:31:59.915Z | 336.951° NNW | 2026-09-22 13:33:59.915Z | 298.115° NW | 28.143° | 2026-09-22 13:36:59.915Z | 238.804° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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