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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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Identifier
62648, 2025-009AR
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
NOVI
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~4 kg wet, ~4 kg dry
Launch date (UTC)
2025-01-14 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 LIME
1 62648U 25009AR  26079.66936264  .00011263  00000-0  40286-3 0  9994
2 62648  97.3976 162.3493 0000586   8.4426 351.6824 15.28962446 65434
Epoch: 2026-03-20T16:03Z
TLE epoch observation values (Epoch: 2026-03-20T16:03:52.932Z)
Latitude
0.00003°
Longitude
103.17764°
Altitude
481.618 km
Speed
7.625 km/s
True Right ascension
10h 49m 23s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:51:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.268 km
Perigee altitude
475.465 km
Semi-major axis
6,854.003 km
Eccentricity
0.00006
Inclination
97.3976°
RAAN
162.3493°
Arg. of periapsis
8.4426°
True anomaly
351.68143°
Mean anomaly
351.6824°
Eccentric anomaly
351.68191°
Mean motion
3.82496 °/min
Orbital period
94.12 mins
BSTAR
0.00040286
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Documentation

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