LEMUR-2 CARROLLEMO, 68489
Orbit data source: Space-Track
LEMUR-2 CARROLLEMO, 68489 is a payload satellite owned by Spire (DE) 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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68489 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated 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, 0.3 m
Radar Cross Section
0.063 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 CARROLLEMO
1 68489U 26067CB 26217.43350115 .00002775 00000-0 27983-3 0 9999
2 68489 97.7564 174.7976 0000185 260.6238 99.4960 14.91924120 19063Epoch: 2026-08-05T10:24Z
TLE epoch observation values (Epoch: 2026-08-05T10:24:14.499Z)
Latitude
-0.00001°
Longitude
64.74922°
Altitude
595 km
Speed
7.562 km/s
True Right ascension
11h 39m 11s
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
12:37:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.084 km
Perigee altitude
588.826 km
Semi-major axis
6,967.092 km
Eccentricity
0.00002
Inclination
97.7564°
RAAN
174.7976°
Arg. of periapsis
260.6238°
True anomaly
99.49809°
Mean anomaly
99.496°
Eccentric anomaly
99.49705°
Mean motion
3.73221 °/min
Orbital period
96.46 mins
BSTAR
0.00027983
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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 CARROLLEMO 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-06 09:30:28.440Z | 32.825° NE | 2026-08-06 09:34:28.440Z | 108.923° ESE | 28.426° | 2026-08-06 09:37:28.440Z | 160.026° S |
| 4 mins | 2026-08-06 20:22:28.440Z | 98.726° ESE | 2026-08-06 20:24:28.440Z | 58.427° ENE | 20.257° | 2026-08-06 20:26:28.440Z | 25.16° NE |
| 5 mins | 2026-08-06 21:57:28.440Z | 220.711° SW | 2026-08-06 21:59:28.440Z | 265.285° W | 25.529° | 2026-08-06 22:02:28.440Z | 319.73° 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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