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 36519U 26131.87359395 +.00000000 +00000-0 +39225-4 0 00004
2 36519 82.9585 276.3887 0035163 229.3746 241.9278 13.71663212 00
| Epoch (UTC): | 11 May 2026 20:57:58 |
| Eccentricity: | 0.0035163 |
| inclination: | 82.9585° |
| perigee height: | 968 km |
| apogee height: | 1020 km |
| right ascension of ascending node: | 276.3887° |
| argument of perigee: | 229.3746° |
| revolutions per day: | 13.71663212 |
| mean anomaly at epoch: | 241.9278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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