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 23090.45369284 .00000402 00000-0 23981-3 0 9996
2 28654 98.9139 165.2102 0013505 237.1036 122.8837 14.12901452920594
| Epoch (UTC): | 31 March 2023 10:53:19 |
| Eccentricity: | 0.0013505 |
| inclination: | 98.9139° |
| perigee height: | 840 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 165.2102° |
| argument of perigee: | 237.1036° |
| revolutions per day: | 14.12901452 |
| mean anomaly at epoch: | 122.8837° |
| orbit number at epoch: | 92059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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