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 Commercial Radar Imaging
Bus & Motor
SSTL-42, Unknown motor
Mass
100 kg wet, 100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Dish, 1.7 m
Radar Cross Section
0.735 m²
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 CARBSAR
1 67397U 26004AL 26146.57566292 .00005835 00000-0 27957-3 0 9999
2 67397 97.4536 146.0184 0007350 62.8694 297.3289 15.19288404 20488Epoch: 2026-05-26T13:48Z
TLE epoch observation values (Epoch: 2026-05-26T13:48:57.276Z)
Latitude
-0.00005°
Longitude
54.63263°
Altitude
508.757 km
Speed
7.611 km/s
True Right ascension
09h 44m 04s
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
06:40:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.018 km
Perigee altitude
499.9 km
Semi-major axis
6,883.096 km
Eccentricity
0.00074
Inclination
97.4536°
RAAN
146.0184°
Arg. of periapsis
62.8694°
True anomaly
297.25404°
Mean anomaly
297.3289°
Eccentric anomaly
297.29148°
Mean motion
3.80073 °/min
Orbital period
94.72 mins
BSTAR
0.00027957
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-26 23:26:07.096Z | 132.469° SE | 2026-05-26 23:29:07.096Z | 69.032° E | 27.421° | 2026-05-26 23:32:07.096Z | 10.205° NNE |
| 6 mins | 2026-05-27 12:31:07.096Z | 29.759° NE | 2026-05-27 12:34:07.096Z | 125.788° SE | 35.197° | 2026-05-27 12:37:07.096Z | 174.776° S |
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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