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OBJECT H, 60242

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 H, 60242 is a payload satellite in LEO that was launched on Tue, 09 Jul 2024 UTC via an ARIANE 62 launch vehicle from the French Guiana (FRGUI). 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
60242, 2024-128H
Orbit
LEO
Country
Flag of TBDTBD
Related business
Manufacturer
PTS
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
24 kg wet, 24 kg dry
Launch date (UTC)
2024-07-09 (2 years ago)
Launch vehicle
ARIANE 62
Launch site
French Guiana (FRGUI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 OBJECT H
1 60242U 24128H   26310.75331632  .00008805  00000-0  48873-3 0  9997
2 60242  61.9787  60.1361 0017708 158.8991 201.2840 15.14263282128030
Epoch: 2026-11-06T18:04Z
TLE epoch observation values (Epoch: 2026-11-06T18:04:46.530Z)
Latitude
0.00001°
Longitude
102.97383°
Altitude
536.386 km
Speed
7.589 km/s
True Right ascension
04h 00m 32s
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
23:39:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.361 km
Perigee altitude
509.923 km
Semi-major axis
6,900.279 km
Eccentricity
0.00177
Inclination
61.9787°
RAAN
60.1361°
Arg. of periapsis
158.8991°
True anomaly
201.21049°
Mean anomaly
201.284°
Eccentric anomaly
201.24723°
Mean motion
3.78655 °/min
Orbital period
95.07 mins
BSTAR
0.00048873
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