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 23081.81414440 .00000302 00000-0 18598-3 0 9998
2 28654 98.9152 156.6081 0013277 263.1871 96.7791 14.12893201919375
| Epoch (UTC): | 22 March 2023 19:32:22 |
| Eccentricity: | 0.0013277 |
| inclination: | 98.9152° |
| perigee height: | 840 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 156.6081° |
| argument of perigee: | 263.1871° |
| revolutions per day: | 14.12893201 |
| mean anomaly at epoch: | 96.7791° |
| orbit number at epoch: | 91937 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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