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 28541U 05004C 23142.16731790 0.00000000 00000-0 00000-0 0 08
2 28541 63.4128 61.0839 0455914 0.1693 359.8911 13.40871754 06
| Epoch (UTC): | 22 May 2023 04:00:56 |
| Eccentricity: | 0.0455914 |
| inclination: | 63.4128° |
| perigee height: | 765 km |
| apogee height: | 1447 km |
| right ascension of ascending node: | 61.0839° |
| argument of perigee: | 0.1693° |
| revolutions per day: | 13.40871754 |
| mean anomaly at epoch: | 359.8911° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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