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 26407U 26145.59801882 +.00000000 +00000-0 +00000-0 0 00001
2 26407 54.8547 216.0596 0121329 302.3746 231.3385 2.00557527 04
| Epoch (UTC): | 25 May 2026 14:21:08 |
| Eccentricity: | 0.0121329 |
| inclination: | 54.8547° |
| perigee height: | 19860 km |
| apogee height: | 20505 km |
| right ascension of ascending node: | 216.0596° |
| argument of perigee: | 302.3746° |
| revolutions per day: | 2.00557527 |
| mean anomaly at epoch: | 231.3385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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