Showing default

GXIBA-1, 67685

Orbit data source: Space-Track

GXIBA-1, 67685 is a payload satellite owned by UPAEP (MX) in LEO that was delivered to the ISS. 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
67685, 1998-067YB
Orbit
LEO
Country
Flag of MXMX / MEX
Related business
Manufacturer
UPAEP
Mission
Operational spacecraft
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
1998-11-20 (28 years ago)
Launch vehicle
H3-24W
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
BOX, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 GXIBA-1
1 67685U 98067YB  26249.38791070  .00058715  00000-0  45324-3 0  9997
2 67685  51.6219 241.4862 0008328 123.2387 236.9410 15.71310362 33013
Epoch: 2026-09-06T09:18Z
TLE epoch observation values (Epoch: 2026-09-06T09:18:35.484Z)
Latitude
-0.00002°
Longitude
116.35459°
Altitude
358.959 km
Speed
7.693 km/s
True Right ascension
16h 05m 56s
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
13:02:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
361.274 km
Perigee altitude
350.059 km
Semi-major axis
6,733.804 km
Eccentricity
0.00083
Inclination
51.6219°
RAAN
241.4862°
Arg. of periapsis
123.2387°
True anomaly
236.86106°
Mean anomaly
236.941°
Eccentric anomaly
236.90103°
Mean motion
3.92783 °/min
Orbital period
91.65 mins
BSTAR
0.00045324
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
|