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 5118U 71028B 23277.76773227 .00014917 00000-0 62594-3 0 9996
2 5118 81.2552 28.7351 0040127 119.6075 240.9165 15.22608516852647
| Epoch (UTC): | 04 October 2023 18:25:32 |
| Eccentricity: | 0.0040127 |
| inclination: | 81.2552° |
| perigee height: | 470 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 28.7351° |
| argument of perigee: | 119.6075° |
| revolutions per day: | 15.22608516 |
| mean anomaly at epoch: | 240.9165° |
| orbit number at epoch: | 85264 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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