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 60905U 26145.62428141 +.00000000 +00000-0 +32890-4 0 00005
2 60905 53.1588 112.3151 0001297 80.4439 279.6725 15.69687361 03
| Epoch (UTC): | 25 May 2026 14:58:57 |
| Eccentricity: | 0.0001297 |
| inclination: | 53.1588° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 112.3151° |
| argument of perigee: | 80.4439° |
| revolutions per day: | 15.69687361 |
| mean anomaly at epoch: | 279.6725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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