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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Edit Public Description
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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LIME
1 62648U 25009AR 25338.47890597 .00026122 00000-0 10184-2 0 9991
2 62648 97.4138 56.9054 0001289 4.7828 355.3423 15.25925565 49225Epoch: 2025-12-04T11:29Z
TLE epoch observation values (Epoch: 2025-12-04T11:29:37.475Z)
Latitude
0.00001°
Longitude
170.96449°
Altitude
490.223 km
Speed
7.62 km/s
True Right ascension
03h 47m 37s
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
09:05:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.85 km
Perigee altitude
484.081 km
Semi-major axis
6,863.103 km
Eccentricity
0.00013
Inclination
97.4138°
RAAN
56.9054°
Arg. of periapsis
4.7828°
True anomaly
355.3411°
Mean anomaly
355.3423°
Eccentric anomaly
355.3417°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.0010184
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
Did you know?
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 | 2025-12-05 17:57:39.983Z | 26.543° NE | 2025-12-05 18:00:39.983Z | 108.277° ESE | 36.775° | 2025-12-05 18:03:39.983Z | 174.116° S |
| 4 mins | 2025-12-06 06:07:39.983Z | 223.26° SW | 2025-12-06 06:09:39.983Z | 272.701° WNW | 22.593° | 2025-12-06 06:11:39.983Z | 313.554° NW |
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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