LIDE, 64869
Orbit data source: Space-Track
LIDE, 64869 is an Italian payload satellite in SSO that was launched on Wed, 23 Jul 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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64869 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
Tyvak Intl
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~15 kg wet, ~15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 LIDE
1 64869U 25154A 26318.20934759 .00002738 00000-0 25444-3 0 9991
2 64869 97.6547 18.5790 0006760 90.4889 269.7106 14.95159878 71411Epoch: 2026-11-14T05:01Z
TLE epoch observation values (Epoch: 2026-11-14T05:01:27.631Z)
Latitude
-0.00009°
Longitude
-110.10353°
Altitude
584.953 km
Speed
7.568 km/s
True Right ascension
01h 14m 18s
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
21:49:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.589 km
Perigee altitude
574.183 km
Semi-major axis
6,957.023 km
Eccentricity
0.00068
Inclination
97.6547°
RAAN
18.579°
Arg. of periapsis
90.4889°
True anomaly
269.63314°
Mean anomaly
269.7106°
Eccentric anomaly
269.67187°
Mean motion
3.74031 °/min
Orbital period
96.25 mins
BSTAR
0.00025444
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Other satellites on launch #154 in the year 2025 (2025-07-23 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.LIDE 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-15 03:38:54.956Z | 131.88° SE | 2026-11-15 03:41:54.956Z | 69.576° E | 35.058° | 2026-11-15 03:44:54.956Z | 10.541° NNE |
| 4 mins | 2026-11-15 05:15:54.956Z | 242.41° WSW | 2026-11-15 05:16:54.956Z | 259.503° W | 16.933° | 2026-11-15 05:19:54.956Z | 307.355° NW |
| 6 mins | 2026-11-15 16:56:54.956Z | 22.041° NNE | 2026-11-15 16:58:54.956Z | 85.352° E | 71.511° | 2026-11-15 17:02:54.956Z | 186.263° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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