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 23082.38263168 .00000040 00000-0 00000-0 0 9991
2 07369 124.8870 117.0650 0067027 3.6240 350.1033 3.07214736546300
| Epoch (UTC): | 23 March 2023 09:10:59 |
| Eccentricity: | 0.0067027 |
| inclination: | 124.8870° |
| perigee height: | 13476 km |
| apogee height: | 13744 km |
| right ascension of ascending node: | 117.0650° |
| argument of perigee: | 3.6240° |
| revolutions per day: | 3.07214736 |
| mean anomaly at epoch: | 350.1033° |
| orbit number at epoch: | 54630 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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