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 26093U 26106.27877078 +.00000000 +00000-0 +29541-3 0 00008
2 26093 100.1830 239.1445 0023559 42.4071 317.8941 14.64911751 07
| Epoch (UTC): | 16 April 2026 06:41:25 |
| Eccentricity: | 0.0023559 |
| inclination: | 100.1830° |
| perigee height: | 661 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 239.1445° |
| argument of perigee: | 42.4071° |
| revolutions per day: | 14.64911751 |
| mean anomaly at epoch: | 317.8941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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