Showing default

IRIDE-MS1-EAG2-16, 68452

Orbit data source: Space-Track

IRIDE-MS1-EAG2-16, 68452 is an Italian payload satellite in SSO that was launched on Mon, 30 Mar 2026 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
68452, 2026-067AN
Orbit
SSO
Country
Flag of ITIT
Related business
Manufacturer
OHB-I
Mission
Operational Commercial Technology
Bus & Motor
EAGLET, Unknown motor
Mass
25 kg wet, 25 kg dry
Launch date (UTC)
2026-03-30 (4 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.368 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 IRIDE-MS1-EAG2-16
1 68452U 26067AN  26219.82899508  .00003914  00000-0  19208-3 0  9995
2 68452  97.4577 177.5281 0002407 218.3728 141.7335 15.18673414 19779
Epoch: 2026-08-07T19:53Z
TLE epoch observation values (Epoch: 2026-08-07T19:53:45.174Z)
Latitude
-0.00009°
Longitude
-77.2592°
Altitude
514.238 km
Speed
7.606 km/s
True Right ascension
11h 50m 06s
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
23:57:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.476 km
Perigee altitude
505.161 km
Semi-major axis
6,884.956 km
Eccentricity
0.00024
Inclination
97.4577°
RAAN
177.5281°
Arg. of periapsis
218.3728°
True anomaly
141.75058°
Mean anomaly
141.7335°
Eccentric anomaly
141.74204°
Mean motion
3.79919 °/min
Orbital period
94.76 mins
BSTAR
0.00019208
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
|