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 36605U 10030A 22176.21557360 .00000002 00000-0 32746-5 0 9990
2 36605 97.4449 183.7039 0002110 81.3980 344.7156 15.19150848666047
| Epoch (UTC): | 25 June 2022 05:10:25 |
| Eccentricity: | 0.0002110 |
| inclination: | 97.4449° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 183.7039° |
| argument of perigee: | 81.3980° |
| revolutions per day: | 15.19150848 |
| mean anomaly at epoch: | 344.7156° |
| orbit number at epoch: | 66604 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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