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: 8 hours ago
TLE from 8 hours ago
0 LEMUR-2 POLO-11
1 68493U 26067CF 26236.61080618 .00003152 00000-0 31429-3 0 9993
2 68493 97.7699 193.8993 0004448 134.1191 226.0395 14.92271850 21921Epoch: 2026-08-24T14:39Z
TLE epoch observation values (Epoch: 2026-08-24T14:39:33.653Z)
Latitude
-0.00001°
Longitude
1.11905°
Altitude
596.049 km
Speed
7.561 km/s
True Right ascension
12h 55m 35s
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
13:53:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.971 km
Perigee altitude
584.774 km
Semi-major axis
6,966.009 km
Eccentricity
0.00044
Inclination
97.7699°
RAAN
193.8993°
Arg. of periapsis
134.1191°
True anomaly
226.00282°
Mean anomaly
226.0395°
Eccentric anomaly
226.02116°
Mean motion
3.73308 °/min
Orbital period
96.44 mins
BSTAR
0.00031429
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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 | 2026-08-25 10:32:54.168Z | 349.954° N | 2026-08-25 10:34:54.168Z | 305.827° NW | 34.54° | 2026-08-25 10:38:54.168Z | 216.009° SW |
| 7 mins | 2026-08-25 21:21:54.168Z | 173.806° S | 2026-08-25 21:24:54.168Z | 265.602° W | 44.091° | 2026-08-25 21:28:54.168Z | 344.206° N |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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