Showing default

CONNECTA IOT-5, 62703

Orbit data source: Space-Track

CONNECTA IOT-5, 62703 is a payload satellite owned by Plan-S (TR) in SSO that was launched on Tue, 14 Jan 2025 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
62703, 2025-009CY
Orbit
SSO
Country
Flag of UnknownUnknown / TURK
Related business
Manufacturer
Plan-S
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
2025-01-14 (11 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 2.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 CONNECTA IOT-5
1 62703U 25009CY  25335.14750496  .00001537  00000-0  14902-3 0  9993
2 62703  97.7214  52.3101 0002643  31.8301 328.3078 14.94117045 47797
Epoch: 2025-12-01T03:32Z
TLE epoch observation values (Epoch: 2025-12-01T03:32:24.428Z)
Latitude
-0.00008°
Longitude
-71.04285°
Altitude
586.595 km
Speed
7.568 km/s
True Right ascension
03h 29m 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
11:45:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.968 km
Perigee altitude
580.289 km
Semi-major axis
6,960.266 km
Eccentricity
0.00026
Inclination
97.7214°
RAAN
52.3101°
Arg. of periapsis
31.8301°
True anomaly
328.29188°
Mean anomaly
328.3078°
Eccentric anomaly
328.29984°
Mean motion
3.7377 °/min
Orbital period
96.32 mins
BSTAR
0.00014902
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
|