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 36089U 26068.48729159 +.00000000 +00000-0 +19394-3 0 00005
2 36089 98.4478 45.5270 0077740 347.2328 12.6896 14.52328349 08
| Epoch (UTC): | 09 March 2026 11:41:41 |
| Eccentricity: | 0.0077740 |
| inclination: | 98.4478° |
| perigee height: | 663 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 45.5270° |
| argument of perigee: | 347.2328° |
| revolutions per day: | 14.52328349 |
| mean anomaly at epoch: | 12.6896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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