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 26069.07580326 +.00000000 +00000-0 +31724-3 0 00007
2 36416 63.3887 313.3327 0690109 2.6477 357.7924 13.72984456 06
| Epoch (UTC): | 10 March 2026 01:49:09 |
| Eccentricity: | 0.0690109 |
| inclination: | 63.3887° |
| perigee height: | 480 km |
| apogee height: | 1497 km |
| right ascension of ascending node: | 313.3327° |
| argument of perigee: | 2.6477° |
| revolutions per day: | 13.72984456 |
| mean anomaly at epoch: | 357.7924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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