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 26070.02264341 +.00000000 +00000-0 +26929-3 0 00001
2 36416 63.3886 310.7572 0690201 2.6550 357.7861 13.72987379 00
| Epoch (UTC): | 11 March 2026 00:32:36 |
| Eccentricity: | 0.0690201 |
| inclination: | 63.3886° |
| perigee height: | 480 km |
| apogee height: | 1497 km |
| right ascension of ascending node: | 310.7572° |
| argument of perigee: | 2.6550° |
| revolutions per day: | 13.72987379 |
| mean anomaly at epoch: | 357.7861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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