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 26068.42029735 +.00000000 +00000-0 +32005-3 0 00000
2 36416 63.3888 315.1157 0690053 2.6435 357.7960 13.72981726 07
| Epoch (UTC): | 09 March 2026 10:05:13 |
| Eccentricity: | 0.0690053 |
| inclination: | 63.3888° |
| perigee height: | 481 km |
| apogee height: | 1497 km |
| right ascension of ascending node: | 315.1157° |
| argument of perigee: | 2.6435° |
| revolutions per day: | 13.72981726 |
| mean anomaly at epoch: | 357.7960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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