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 23342.18901393 .00000201 00000-0 13130-3 0 9991
2 28654 98.8954 55.6136 0013454 245.3419 114.6352 14.13073488956147
| Epoch (UTC): | 08 December 2023 04:32:10 |
| Eccentricity: | 0.0013454 |
| inclination: | 98.8954° |
| perigee height: | 839 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 55.6136° |
| argument of perigee: | 245.3419° |
| revolutions per day: | 14.13073488 |
| mean anomaly at epoch: | 114.6352° |
| orbit number at epoch: | 95614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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