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, 0.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 LEMUR-2 CARROLLEMO
1 68489U 26067CB 26262.63514149 .00002350 00000-0 23660-3 0 9997
2 68489 97.7634 219.3174 0003746 100.2327 259.9314 14.92119981 25808Epoch: 2026-09-19T15:14Z
TLE epoch observation values (Epoch: 2026-09-19T15:14:36.224Z)
Latitude
-0.00009°
Longitude
-7.87437°
Altitude
594.826 km
Speed
7.562 km/s
True Right ascension
14h 37m 16s
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
03:11:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.955 km
Perigee altitude
585.735 km
Semi-major axis
6,966.482 km
Eccentricity
0.00037
Inclination
97.7634°
RAAN
219.3174°
Arg. of periapsis
100.2327°
True anomaly
259.88914°
Mean anomaly
259.9314°
Eccentric anomaly
259.91027°
Mean motion
3.7327 °/min
Orbital period
96.44 mins
BSTAR
0.0002366
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-20 11:07:37.500Z | 330.333° NNW | 2026-09-20 11:09:37.500Z | 297.769° NW | 18.858° | 2026-09-20 11:12:37.500Z | 249.746° W |
| 5 mins | 2026-09-20 20:22:37.500Z | 102.32° ESE | 2026-09-20 20:24:37.500Z | 63.014° ENE | 22.262° | 2026-09-20 20:27:37.500Z | 17.092° NNE |
| 5 mins | 2026-09-20 21:57:37.500Z | 218.142° SW | 2026-09-20 21:59:37.500Z | 259.829° W | 28.235° | 2026-09-20 22:02:37.500Z | 317.545° NNW |
| 6 mins | 2026-09-21 09:40:37.500Z | 37.599° NE | 2026-09-21 09:42:37.500Z | 82.496° E | 41.431° | 2026-09-21 09:46:37.500Z | 169.217° S |
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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