LEMUR 2 HUBBLE-5, 64840
Orbit data source: Space-Track
LEMUR 2 HUBBLE-5, 64840 is an American payload satellite in SSO that was launched on Mon, 23 Jun 2025 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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64840 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 1.4 m
Radar Cross Section
0.326 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 HUBBLE-5
1 64840U 25135BT 26289.56099626 .00001145 00000-0 11154-3 0 9994
2 64840 97.7824 42.9218 0004279 302.0414 58.0390 14.94437128 72033Epoch: 2026-10-16T13:27Z
TLE epoch observation values (Epoch: 2026-10-16T13:27:50.076Z)
Latitude
-0.00007°
Longitude
175.88291°
Altitude
585.589 km
Speed
7.568 km/s
True Right ascension
02h 51m 41s
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
04:07:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.115 km
Perigee altitude
578.159 km
Semi-major axis
6,959.274 km
Eccentricity
0.00043
Inclination
97.7824°
RAAN
42.9218°
Arg. of periapsis
302.0414°
True anomaly
58.08061°
Mean anomaly
58.039°
Eccentric anomaly
58.05981°
Mean motion
3.7385 °/min
Orbital period
96.3 mins
BSTAR
0.00011154
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Other satellites on launch #135 in the year 2025 (2025-06-23 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 HUBBLE-5 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 | 2026-10-17 20:33:29.163Z | 12.873° NNE | 2026-10-17 20:37:29.163Z | 185.55° SSW | 76.131° | 2026-10-17 20:40:29.163Z | 192.684° SSW |
| 6 mins | 2026-10-18 07:23:29.163Z | 139.189° SSE | 2026-10-18 07:25:29.163Z | 85.084° E | 50.843° | 2026-10-18 07:29:29.163Z | 358.869° 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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