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 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, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LEMUR-2 CARROLLEMO
1 68489U 26067CB 26171.35305110 .00002853 00000-0 28942-3 0 9997
2 68489 97.7535 129.4566 0003845 72.1808 287.9830 14.91654326 12193Epoch: 2026-06-20T08:28Z
TLE epoch observation values (Epoch: 2026-06-20T08:28:23.615Z)
Latitude
0.00001°
Longitude
93.78931°
Altitude
594.992 km
Speed
7.563 km/s
True Right ascension
08h 37m 49s
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
07:12:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.475 km
Perigee altitude
587.116 km
Semi-major axis
6,967.933 km
Eccentricity
0.00038
Inclination
97.7535°
RAAN
129.4566°
Arg. of periapsis
72.1808°
True anomaly
287.94109°
Mean anomaly
287.983°
Eccentric anomaly
287.96204°
Mean motion
3.73153 °/min
Orbital period
96.48 mins
BSTAR
0.00028942
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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 | 2026-06-20 21:27:54.580Z | 178.593° S | 2026-06-20 21:31:54.580Z | 267.261° W | 41.177° | 2026-06-20 21:34:54.580Z | 337.163° NNW |
| 4 mins | 2026-06-21 09:13:54.580Z | 69.533° E | 2026-06-21 09:14:54.580Z | 88.675° E | 19.265° | 2026-06-21 09:17:54.580Z | 139.424° SSE |
| 5 mins | 2026-06-21 10:48:54.580Z | 332.325° NNW | 2026-06-21 10:50:54.580Z | 285.505° WNW | 26.525° | 2026-06-21 10:53:54.580Z | 232.124° WSW |
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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