CARBSAR, 67397
Orbit data source: Space-Track
CARBSAR, 67397 is a payload satellite owned by SSTL (UK) 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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67397 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
SSTL
Mission
Operational spacecraft
Bus & Motor
SSTL-42, Unknown motor
Mass
100 kg wet, 100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.9 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 CARBSAR
1 67397U 26004AL 26093.61280336 .00012180 00000-0 58952-3 0 9997
2 67397 97.4547 93.7556 0004378 222.6848 137.4047 15.18713536 12446Epoch: 2026-04-03T14:42Z
TLE epoch observation values (Epoch: 2026-04-03T14:42:26.210Z)
Latitude
0.00002°
Longitude
41.20196°
Altitude
515.036 km
Speed
7.605 km/s
True Right ascension
06h 15m 01s
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
03:50:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.711 km
Perigee altitude
503.683 km
Semi-major axis
6,884.834 km
Eccentricity
0.00044
Inclination
97.4547°
RAAN
93.7556°
Arg. of periapsis
222.6848°
True anomaly
137.43864°
Mean anomaly
137.4047°
Eccentric anomaly
137.42167°
Mean motion
3.79929 °/min
Orbital period
94.75 mins
BSTAR
0.00058952
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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.CARBSAR 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 | 2026-04-04 00:20:16.234Z | 197.803° SSW | 2026-04-04 00:22:16.234Z | 269.641° W | 36.586° | 2026-04-04 00:25:16.234Z | 334.219° NNW |
| 5 mins | 2026-04-04 13:25:16.234Z | 334.94° NNW | 2026-04-04 13:27:16.234Z | 280.762° WNW | 27.246° | 2026-04-04 13:30:16.234Z | 225.567° 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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