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 15369U 84111A 22230.23286730 .00003695 00000-0 17391-3 0 9996
2 15369 82.5250 62.0663 0016566 176.2402 183.8961 15.19119676 66641
| Epoch (UTC): | 18 August 2022 05:35:19 |
| Eccentricity: | 0.0016566 |
| inclination: | 82.5250° |
| perigee height: | 497 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 62.0663° |
| argument of perigee: | 176.2402° |
| revolutions per day: | 15.19119676 |
| mean anomaly at epoch: | 183.8961° |
| orbit number at epoch: | 6664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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