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 10517U 77118B 23271.94689047 .00001820 00000-0 31876-3 0 9999
2 10517 28.6655 71.2904 0835209 272.2183 78.3071 13.42458556217237
| Epoch (UTC): | 28 September 2023 22:43:31 |
| Eccentricity: | 0.0835209 |
| inclination: | 28.6655° |
| perigee height: | 475 km |
| apogee height: | 1725 km |
| right ascension of ascending node: | 71.2904° |
| argument of perigee: | 272.2183° |
| revolutions per day: | 13.42458556 |
| mean anomaly at epoch: | 78.3071° |
| orbit number at epoch: | 21723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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