LIME, 62648
Orbit data source: Space-Track
LIME, 62648 is an American payload satellite in SSO that was launched on Tue, 14 Jan 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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62648 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NOVI
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~4 kg wet, ~4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 LIME
1 62648U 25009AR 26215.20708304 .00009891 00000-0 32462-3 0 9999
2 62648 97.3932 297.3616 0002661 141.0649 219.0784 15.31793031 86160Epoch: 2026-08-03T04:58Z
TLE epoch observation values (Epoch: 2026-08-03T04:58:11.974Z)
Latitude
-0.00009°
Longitude
-88.98179°
Altitude
474.985 km
Speed
7.628 km/s
True Right ascension
19h 49m 26s
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
17:51:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.234 km
Perigee altitude
465.591 km
Semi-major axis
6,845.549 km
Eccentricity
0.00027
Inclination
97.3932°
RAAN
297.3616°
Arg. of periapsis
141.0649°
True anomaly
219.05918°
Mean anomaly
219.0784°
Eccentric anomaly
219.06879°
Mean motion
3.83205 °/min
Orbital period
93.94 mins
BSTAR
0.00032462
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.LIME 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 | 2026-08-05 05:41:54.029Z | 174.823° S | 2026-08-05 05:44:54.029Z | 288.367° WNW | 43.121° | 2026-08-05 05:47:54.029Z | 343.33° N |
| 5 mins | 2026-08-05 18:40:54.029Z | 355.738° N | 2026-08-05 18:42:54.029Z | 298.179° NW | 38.378° | 2026-08-05 18:45:54.029Z | 209.955° SW |
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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