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OBJECT E, 61242

Orbit data source: Space-Track

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Recently launched and/or uncataloged RSOs may have evolving metadata. Metadata may include the following, but is not limited to: Owner, Manufacturer, Bus, Motor, and Mission.

OBJECT E, 61242 is a Chinese payload satellite in SSO that was launched on Tue, 24 Sep 2024 UTC via a LIJIAN-1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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
61242, 2024-174E
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
Unknown
Mission
Operational Commercial Meteo Radio Occ.
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2024-09-24 (2 years ago)
Launch vehicle
LIJIAN-1
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 2.5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 OBJECT E
1 61242U 24174E   26317.74456412  .00006277  00000-0  22430-3 0  9991
2 61242  97.4438 328.6688 0014413  68.4393 291.8381 15.29094344118686
Epoch: 2026-11-13T17:52Z
TLE epoch observation values (Epoch: 2026-11-13T17:52:10.339Z)
Latitude
-0.0001°
Longitude
7.76643°
Altitude
477.955 km
Speed
7.629 km/s
True Right ascension
21h 54m 40s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
20:55:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.352 km
Perigee altitude
465.596 km
Semi-major axis
6,853.611 km
Eccentricity
0.00144
Inclination
97.4438°
RAAN
328.6688°
Arg. of periapsis
68.4393°
True anomaly
291.68469°
Mean anomaly
291.8381°
Eccentric anomaly
291.7614°
Mean motion
3.82529 °/min
Orbital period
94.11 mins
BSTAR
0.0002243
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