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 23628U 95038A 23080.77938953 -.00000111 00000-0 00000-0 0 9994
2 23628 12.3220 23.2538 0002399 97.8294 84.3509 0.98663667 21089
| Epoch (UTC): | 21 March 2023 18:42:19 |
| Eccentricity: | 0.0002399 |
| inclination: | 12.3220° |
| perigee height: | 36233 km |
| apogee height: | 36253 km |
| right ascension of ascending node: | 23.2538° |
| argument of perigee: | 97.8294° |
| revolutions per day: | 0.98663667 |
| mean anomaly at epoch: | 84.3509° |
| orbit number at epoch: | 2108 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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