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: 11 hours ago
TLE from 11 hours ago
0 LEMUR 2 HUBBLE-5
1 64840U 25135BT 26178.26979266 .00001974 00000-0 18975-3 0 9993
2 64840 97.7726 292.7043 0004272 315.2730 44.8145 14.94165966 55417Epoch: 2026-06-27T06:28Z
TLE epoch observation values (Epoch: 2026-06-27T06:28:30.085Z)
Latitude
-0.00005°
Longitude
-79.80741°
Altitude
585.897 km
Speed
7.568 km/s
True Right ascension
19h 30m 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
05:12:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.952 km
Perigee altitude
579.006 km
Semi-major axis
6,960.116 km
Eccentricity
0.00043
Inclination
97.7726°
RAAN
292.7043°
Arg. of periapsis
315.273°
True anomaly
44.84902°
Mean anomaly
44.8145°
Eccentric anomaly
44.83176°
Mean motion
3.73782 °/min
Orbital period
96.31 mins
BSTAR
0.00018975
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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 | 2026-06-27 19:54:12.504Z | 34.987° NE | 2026-06-27 19:57:12.504Z | 82.581° E | 26.677° | 2026-06-27 20:01:12.504Z | 159.05° S |
| 4 mins | 2026-06-27 21:31:12.504Z | 323.712° NNW | 2026-06-27 21:33:12.504Z | 286.156° WNW | 18.944° | 2026-06-27 21:35:12.504Z | 252.721° W |
| 4 mins | 2026-06-28 06:45:12.504Z | 95.55° ESE | 2026-06-28 06:46:12.504Z | 77.264° E | 18.691° | 2026-06-28 06:49:12.504Z | 25.332° NE |
| 5 mins | 2026-06-28 08:20:12.504Z | 221.786° SW | 2026-06-28 08:22:12.504Z | 272.581° WNW | 26.915° | 2026-06-28 08:25:12.504Z | 323.712° 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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