APEX ARIES 1, 59129

Orbit data source: Space-Track

APEX ARIES 1, 59129 is a payload satellite owned by Apex (US) in SSO that was launched on Mon, 04 Mar 2024 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.

Loading next visibility...
Identifier
59129, 2024-043AH
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Apex
Mission
Operational Commercial Technology
Bus & Motor
ARIES, Unknown motor
Mass
200 kg wet, 200 kg dry
Launch date (UTC)
2024-03-04 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.8 m
Radar Cross Section
1.983 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 APEX ARIES 1
1 59129U 24043AH  25289.13393884  .00023911  00000-0  57392-3 0  9999
2 59129  97.5233  63.8119 0007399  10.1443 349.9951 15.41341138 90141
Epoch: 2025-10-16T03:12Z
TLE epoch observation values (Epoch: 2025-10-16T03:12:52.315Z)
Latitude
-0.00007°
Longitude
-9.3041°
Altitude
440.295 km
Speed
7.651 km/s
True Right ascension
04h 15m 14s
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
05:01:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
444.137 km
Perigee altitude
434.049 km
Semi-major axis
6,817.23 km
Eccentricity
0.00074
Inclination
97.5233°
RAAN
63.8119°
Arg. of periapsis
10.1443°
True anomaly
349.98036°
Mean anomaly
349.9951°
Eccentric anomaly
349.98773°
Mean motion
3.85595 °/min
Orbital period
93.36 mins
BSTAR
0.00057392
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|