LEMUR-2 KUTAR, 67394
Orbit data source: Space-Track
LEMUR-2 KUTAR, 67394 is a payload satellite owned by Spire (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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67394 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.115 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LEMUR-2 KUTAR
1 67394U 26004AH 26206.42032851 .00004508 00000-0 21413-3 0 9993
2 67394 97.4508 205.0162 0008143 190.3979 169.7089 15.19707759 29578Epoch: 2026-07-25T10:05Z
TLE epoch observation values (Epoch: 2026-07-25T10:05:16.383Z)
Latitude
0.00002°
Longitude
110.56507°
Altitude
515.329 km
Speed
7.603 km/s
True Right ascension
13h 40m 03s
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
11:11:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.295 km
Perigee altitude
498.087 km
Semi-major axis
6,881.828 km
Eccentricity
0.00081
Inclination
97.4508°
RAAN
205.0162°
Arg. of periapsis
190.3979°
True anomaly
169.72555°
Mean anomaly
169.7089°
Eccentric anomaly
169.71723°
Mean motion
3.80178 °/min
Orbital period
94.69 mins
BSTAR
0.00021413
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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.LEMUR-2 KUTAR 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 | 2026-07-26 00:26:59.618Z | 204.264° SW | 2026-07-26 00:28:59.618Z | 262.317° W | 32.346° | 2026-07-26 00:31:59.618Z | 329.084° NNW |
| 4 mins | 2026-07-26 11:57:59.618Z | 64.575° ENE | 2026-07-26 11:58:59.618Z | 83.548° E | 16.699° | 2026-07-26 12:01:59.618Z | 137.952° SSE |
| 4 mins | 2026-07-26 13:31:59.618Z | 323.912° NNW | 2026-07-26 13:32:59.618Z | 299.554° NW | 23.501° | 2026-07-26 13:35:59.618Z | 235.598° 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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