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 36416U 26064.41439914 +.00000000 +00000-0 +42938-3 0 00005
2 36416 63.3896 326.0112 0689732 2.6157 357.8200 13.72965731 07
| Epoch (UTC): | 05 March 2026 09:56:44 |
| Eccentricity: | 0.0689732 |
| inclination: | 63.3896° |
| perigee height: | 481 km |
| apogee height: | 1497 km |
| right ascension of ascending node: | 326.0112° |
| argument of perigee: | 2.6157° |
| revolutions per day: | 13.72965731 |
| mean anomaly at epoch: | 357.8200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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