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 65054U 26088.11839344 +.00000000 +00000-0 +11989-3 0 00001
2 65054 98.4364 279.3613 0010844 295.5816 64.4255 14.47783835 06
| Epoch (UTC): | 29 March 2026 02:50:29 |
| Eccentricity: | 0.0010844 |
| inclination: | 98.4364° |
| perigee height: | 725 km |
| apogee height: | 741 km |
| right ascension of ascending node: | 279.3613° |
| argument of perigee: | 295.5816° |
| revolutions per day: | 14.47783835 |
| mean anomaly at epoch: | 64.4255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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