LEMUR-2 POLO-11, 68493
Orbit data source: Space-Track
LEMUR-2 POLO-11, 68493 is a payload satellite owned by Spire (LU) in SSO that was launched on Mon, 30 Mar 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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68493 intel report (Beta)
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Identifier
Orbit
Country
LU / LUXERelated business
Manufacturer
Spire/Glasgow
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 LEMUR-2 POLO-11
1 68493U 26067CF 26171.42479104 .00005389 00000-0 54070-3 0 9993
2 68493 97.7652 129.6300 0004680 39.9353 320.2209 14.91714361 12209Epoch: 2026-06-20T10:11Z
TLE epoch observation values (Epoch: 2026-06-20T10:11:41.945Z)
Latitude
-0.00007°
Longitude
68.06563°
Altitude
593.124 km
Speed
7.565 km/s
True Right ascension
08h 38m 31s
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
16:36:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.87 km
Perigee altitude
586.348 km
Semi-major axis
6,967.746 km
Eccentricity
0.00047
Inclination
97.7652°
RAAN
129.63°
Arg. of periapsis
39.9353°
True anomaly
320.18657°
Mean anomaly
320.2209°
Eccentric anomaly
320.20374°
Mean motion
3.73168 °/min
Orbital period
96.47 mins
BSTAR
0.0005407
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Other satellites on launch #67 in the year 2026 (2026-03-30 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 POLO-11 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 | 2026-06-22 09:27:58.497Z | 43.285° NE | 2026-06-22 09:30:58.497Z | 106.247° ESE | 26.288° | 2026-06-22 09:33:58.497Z | 156.389° SSE |
| 5 mins | 2026-06-22 11:03:58.497Z | 329.019° NNW | 2026-06-22 11:05:58.497Z | 292.943° NW | 19.856° | 2026-06-22 11:08:58.497Z | 244.531° WSW |
| 4 mins | 2026-06-22 20:18:58.497Z | 99.048° ESE | 2026-06-22 20:20:58.497Z | 61.925° ENE | 18.771° | 2026-06-22 20:22:58.497Z | 28.542° NE |
| 5 mins | 2026-06-22 21:53:58.497Z | 215.117° SW | 2026-06-22 21:55:58.497Z | 260.721° W | 27.599° | 2026-06-22 21:58:58.497Z | 320.562° NNW |
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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