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: 9 hours ago

TLE from 9 hours ago
0 GXIBA-1
1 67685U 98067YB  26223.79201895  .00042141  00000-0  37775-3 0  9992
2 67685  51.6251  12.0899 0007535  42.4883 317.6695 15.67842533 28991
Epoch: 2026-08-11T19:00Z
TLE epoch observation values (Epoch: 2026-08-11T19:00:30.437Z)
Latitude
-0.00004°
Longitude
126.70782°
Altitude
362.067 km
Speed
7.696 km/s
True Right ascension
00h 48m 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
18:46:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
370.672 km
Perigee altitude
360.509 km
Semi-major axis
6,743.727 km
Eccentricity
0.00075
Inclination
51.6251°
RAAN
12.0899°
Arg. of periapsis
42.4883°
True anomaly
317.61131°
Mean anomaly
317.6695°
Eccentric anomaly
317.64041°
Mean motion
3.91916 °/min
Orbital period
91.86 mins
BSTAR
0.00037775
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|