View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 67259U 26144.15748535 +.00000000 +00000-0 +44613-3 0 00008
2 67259 97.3973 219.3868 0015941 88.6934 271.6129 15.23881454 03
| Epoch (UTC): | 24 May 2026 03:46:46 |
| Eccentricity: | 0.0015941 |
| inclination: | 97.3973° |
| perigee height: | 483 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 219.3868° |
| argument of perigee: | 88.6934° |
| revolutions per day: | 15.23881454 |
| mean anomaly at epoch: | 271.6129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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