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 23334.11698304 .00000433 00000-0 25542-3 0 9997
2 28654 98.8959 47.5930 0013338 269.8956 90.0687 14.13067181955007
| Epoch (UTC): | 30 November 2023 02:48:27 |
| Eccentricity: | 0.0013338 |
| inclination: | 98.8959° |
| perigee height: | 839 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 47.5930° |
| argument of perigee: | 269.8956° |
| revolutions per day: | 14.13067181 |
| mean anomaly at epoch: | 90.0687° |
| orbit number at epoch: | 95500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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