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 (27 years ago)
Launch vehicle
H3-24W
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown

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

TLE from 12 hours ago
0 GXIBA-1
1 67685U 98067YB  26111.99544376  .00040871  00000-0  57561-3 0  9997
2 67685  51.6289 215.8397 0013967 346.7819  13.2804 15.56112947 11522
Epoch: 2026-04-21T23:53Z
TLE epoch observation values (Epoch: 2026-04-21T23:53:26.340Z)
Latitude
-0.00008°
Longitude
7.41666°
Altitude
390.45 km
Speed
7.682 km/s
True Right ascension
14h 23m 21s
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
18:41:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
408.897 km
Perigee altitude
389.964 km
Semi-major axis
6,777.567 km
Eccentricity
0.0014
Inclination
51.6289°
RAAN
215.8397°
Arg. of periapsis
346.7819°
True anomaly
13.31723°
Mean anomaly
13.2804°
Eccentric anomaly
13.29881°
Mean motion
3.88985 °/min
Orbital period
92.55 mins
BSTAR
0.00057561
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|