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 36415U 26145.14176126 +.00000000 +00000-0 +11133-3 0 00000
2 36415 63.3669 58.0052 0537125 21.0550 341.1702 13.45706360 03
| Epoch (UTC): | 25 May 2026 03:24:08 |
| Eccentricity: | 0.0537125 |
| inclination: | 63.3669° |
| perigee height: | 687 km |
| apogee height: | 1489 km |
| right ascension of ascending node: | 58.0052° |
| argument of perigee: | 21.0550° |
| revolutions per day: | 13.45706360 |
| mean anomaly at epoch: | 341.1702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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