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 Commercial Com/MetRO
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
Box + 2 Pan, 0.2 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 LEMUR-2 POLO-11
1 68493U 26067CF 26201.87480976 .00003868 00000-0 38679-3 0 9992
2 68493 97.7665 159.6393 0001801 282.5149 77.5869 14.92024730 16741Epoch: 2026-07-20T20:59Z
TLE epoch observation values (Epoch: 2026-07-20T20:59:43.563Z)
Latitude
0.00005°
Longitude
-93.94481°
Altitude
594.395 km
Speed
7.563 km/s
True Right ascension
10h 38m 33s
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
06:07:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.897 km
Perigee altitude
587.387 km
Semi-major axis
6,966.779 km
Eccentricity
0.00018
Inclination
97.7665°
RAAN
159.6393°
Arg. of periapsis
282.5149°
True anomaly
77.60706°
Mean anomaly
77.5869°
Eccentric anomaly
77.59698°
Mean motion
3.73246 °/min
Orbital period
96.45 mins
BSTAR
0.00038679
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-07-21 21:15:04.569Z | 167.115° S | 2026-07-21 21:19:04.569Z | 227.582° WSW | 44.981° | 2026-07-21 21:23:04.569Z | 347.233° N |
| 6 mins | 2026-07-22 10:35:04.569Z | 351.956° N | 2026-07-22 10:38:04.569Z | 282.422° WNW | 33.819° | 2026-07-22 10:41:04.569Z | 221.102° SW |
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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