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, 0.7 m
Radar Cross Section
0.078 m²
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 BLACKCAT
1 67369U 26004G 26146.56283614 .00001450 00000-0 16552-3 0 9999
2 67369 97.7982 145.3725 0006310 203.7534 156.3392 14.87583714 20072Epoch: 2026-05-26T13:30Z
TLE epoch observation values (Epoch: 2026-05-26T13:30:29.042Z)
Latitude
-0.00002°
Longitude
58.61701°
Altitude
612.56 km
Speed
7.551 km/s
True Right ascension
09h 41m 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
06:41:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
606.919 km
Perigee altitude
598.109 km
Semi-major axis
6,980.651 km
Eccentricity
0.00063
Inclination
97.7982°
RAAN
145.3725°
Arg. of periapsis
203.7534°
True anomaly
156.3682°
Mean anomaly
156.3392°
Eccentric anomaly
156.3537°
Mean motion
3.72134 °/min
Orbital period
96.74 mins
BSTAR
0.00016552
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-26 23:19:20.086Z | 134.993° SE | 2026-05-26 23:23:20.086Z | 60.674° ENE | 29.106° | 2026-05-26 23:26:20.086Z | 9.536° NNE |
| 4 mins | 2026-05-27 00:57:20.086Z | 238.808° WSW | 2026-05-27 00:59:20.086Z | 274.543° WNW | 17.698° | 2026-05-27 01:01:20.086Z | 305.601° NW |
| 7 mins | 2026-05-27 12:41:20.086Z | 18.866° NNE | 2026-05-27 12:44:20.086Z | 124.221° SE | 43.684° | 2026-05-27 12:48:20.086Z | 187.408° SSW |
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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