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 23054.76142140 0.00000200 00000-0 20003-3 0 01
2 28541 63.4078 284.6873 0448388 0.0901 359.9099 13.40870824 04
| Epoch (UTC): | 23 February 2023 18:16:26 |
| Eccentricity: | 0.0448388 |
| inclination: | 63.4078° |
| perigee height: | 770 km |
| apogee height: | 1441 km |
| right ascension of ascending node: | 284.6873° |
| argument of perigee: | 0.0901° |
| revolutions per day: | 13.40870824 |
| mean anomaly at epoch: | 359.9099° |
| 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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