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 39316U 94029AFB 23086.24236816 .00063886 00000-0 23081-2 0 9994
2 39316 81.9913 181.7307 0043915 235.0661 124.6448 15.27272790 39639
| Epoch (UTC): | 27 March 2023 05:49:00 |
| Eccentricity: | 0.0043915 |
| inclination: | 81.9913° |
| perigee height: | 454 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 181.7307° |
| argument of perigee: | 235.0661° |
| revolutions per day: | 15.27272790 |
| mean anomaly at epoch: | 124.6448° |
| orbit number at epoch: | 3963 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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