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 36414U 26145.21776480 +.00000000 +00000-0 +11661-3 0 00002
2 36414 63.3674 57.2951 0536439 20.7243 341.4661 13.45704828 03
| Epoch (UTC): | 25 May 2026 05:13:34 |
| Eccentricity: | 0.0536439 |
| inclination: | 63.3674° |
| perigee height: | 688 km |
| apogee height: | 1489 km |
| right ascension of ascending node: | 57.2951° |
| argument of perigee: | 20.7243° |
| revolutions per day: | 13.45704828 |
| mean anomaly at epoch: | 341.4661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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