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 26064.92424338 +.00000000 +00000-0 +36039-3 0 00000
2 36416 63.3895 324.6246 0689774 2.6191 357.8171 13.72967115 07
| Epoch (UTC): | 05 March 2026 22:10:54 |
| Eccentricity: | 0.0689774 |
| inclination: | 63.3895° |
| perigee height: | 481 km |
| apogee height: | 1497 km |
| right ascension of ascending node: | 324.6246° |
| argument of perigee: | 2.6191° |
| revolutions per day: | 13.72967115 |
| mean anomaly at epoch: | 357.8171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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