Showing default

MOI-1A, 101107

Orbit data source: Space-Track

MOI-1A, 101107 is an Indian payload satellite in SSO that was launched on Thu, 01 Oct 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
101107, 2026-227CV
Orbit
SSO
Country
Flag of ININ / IND
Related business
None
Manufacturer
ISRO
Mission
Operational spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
13 kg wet, 13 kg dry
Launch date (UTC)
2026-10-01 (1 month ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
BOX, 0.2 m
Radar Cross Section
RCS unknown

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

TLE from 9 hours ago
0 MOI-1A
1 A1107U 26227CV  26302.98124265  .00004893  00000-0  25284-3 0  9996
2 A1107  97.4385  11.9761 0005497  97.6924 262.4934 15.16729043  4286
Epoch: 2026-10-29T23:32Z
TLE epoch observation values (Epoch: 2026-10-29T23:32:59.364Z)
Latitude
-0.00002°
Longitude
-19.57912°
Altitude
519.317 km
Speed
7.603 km/s
True Right ascension
00h 47m 54s
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
03:40:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.494 km
Perigee altitude
508.918 km
Semi-major axis
6,890.843 km
Eccentricity
0.00055
Inclination
97.4385°
RAAN
11.9761°
Arg. of periapsis
97.6924°
True anomaly
262.43095°
Mean anomaly
262.4934°
Eccentric anomaly
262.46218°
Mean motion
3.79433 °/min
Orbital period
94.88 mins
BSTAR
0.00025284
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
|