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 23336.45362546 .00000703 00000-0 40031-3 0 9992
2 28654 98.8957 49.9148 0013333 262.6440 97.3216 14.13071727955331
| Epoch (UTC): | 02 December 2023 10:53:13 |
| Eccentricity: | 0.0013333 |
| inclination: | 98.8957° |
| perigee height: | 839 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 49.9148° |
| argument of perigee: | 262.6440° |
| revolutions per day: | 14.13071727 |
| mean anomaly at epoch: | 97.3216° |
| orbit number at epoch: | 95533 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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