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 07369U 74054A 23269.37877865 .00000047 00000-0 00000-0 0 9999
2 07369 124.7826 136.8058 0065733 16.4926 160.6710 3.07214505552055
| Epoch (UTC): | 26 September 2023 09:05:26 |
| Eccentricity: | 0.0065733 |
| inclination: | 124.7826° |
| perigee height: | 13478 km |
| apogee height: | 13741 km |
| right ascension of ascending node: | 136.8058° |
| argument of perigee: | 16.4926° |
| revolutions per day: | 3.07214505 |
| mean anomaly at epoch: | 160.6710° |
| orbit number at epoch: | 55205 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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