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 data is extracted from the following two-line orbital elements,
1 36519U 10017A 22225.91629029 .00000024 00000-0 97736-5 0 9997
2 36519 82.9607 200.5951 0037592 64.4983 324.2745 13.71477717615576
| Epoch (UTC): | 13 August 2022 21:59:27 |
| Eccentricity: | 0.0037592 |
| inclination: | 82.9607° |
| perigee height: | 966 km |
| apogee height: | 1022 km |
| right ascension of ascending node: | 200.5951° |
| argument of perigee: | 64.4983° |
| revolutions per day: | 13.71477717 |
| mean anomaly at epoch: | 324.2745° |
| orbit number at epoch: | 61557 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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