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 28654U 05018A 23340.77287019 .00000279 00000-0 17333-3 0 9990
2 28654 98.8955 54.2065 0013407 249.6298 110.3434 14.13072777955945
| Epoch (UTC): | 06 December 2023 18:32:55 |
| Eccentricity: | 0.0013407 |
| inclination: | 98.8955° |
| perigee height: | 839 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 54.2065° |
| argument of perigee: | 249.6298° |
| revolutions per day: | 14.13072777 |
| mean anomaly at epoch: | 110.3434° |
| orbit number at epoch: | 95594 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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