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 36039U 09059D 22226.38178398 .00000586 00000-0 59502-4 0 9999
2 36039 98.4122 17.5267 0136626 262.0582 96.5109 14.88879577693435
| Epoch (UTC): | 14 August 2022 09:09:46 |
| Eccentricity: | 0.0136626 |
| inclination: | 98.4122° |
| perigee height: | 506 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 17.5267° |
| argument of perigee: | 262.0582° |
| revolutions per day: | 14.88879577 |
| mean anomaly at epoch: | 96.5109° |
| orbit number at epoch: | 69343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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