UMBRA-12, 67371
Orbit data source: Space-Track
UMBRA-12, 67371 is a payload satellite owned by Umbra Labs (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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67371 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Umbra Labs
Mission
Operational Commercial Radar Imaging
Bus & Motor
ESPASAT?, Unknown motor
Mass
84 kg wet, 79 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan + 1 Dish, 1.2 m
Radar Cross Section
1.219 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 UMBRA-12
1 67371U 26004J 26206.60102633 .00004852 00000-0 51359-3 0 9998
2 67371 97.8029 204.8480 0006489 24.3070 335.8453 14.89604039 29028Epoch: 2026-07-25T14:25Z
TLE epoch observation values (Epoch: 2026-07-25T14:25:28.674Z)
Latitude
0.00001°
Longitude
45.16755°
Altitude
598.078 km
Speed
7.563 km/s
True Right ascension
13h 39m 23s
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
10:26:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
600.721 km
Perigee altitude
591.67 km
Semi-major axis
6,974.333 km
Eccentricity
0.00065
Inclination
97.8029°
RAAN
204.848°
Arg. of periapsis
24.307°
True anomaly
335.81485°
Mean anomaly
335.8453°
Eccentric anomaly
335.83008°
Mean motion
3.7264 °/min
Orbital period
96.61 mins
BSTAR
0.00051359
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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.UMBRA-12 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 | 2026-07-26 00:14:11.275Z | 188.522° SSW | 2026-07-26 00:16:11.275Z | 239.488° WSW | 39.623° | 2026-07-26 00:20:11.275Z | 337.965° N |
| 4 mins | 2026-07-26 11:59:11.275Z | 62.567° ENE | 2026-07-26 12:01:11.275Z | 102.431° ESE | 20.721° | 2026-07-26 12:03:11.275Z | 137.045° SSE |
| 5 mins | 2026-07-26 13:34:11.275Z | 337.222° NNW | 2026-07-26 13:36:11.275Z | 298.533° NW | 25.151° | 2026-07-26 13:39:11.275Z | 238.889° WSW |
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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