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 28537U 05004A 23054.76133415 0.00000200 00000-0 20050-3 0 03
2 28537 63.4078 284.4655 0447509 0.2604 359.7396 13.40871153 05
| Epoch (UTC): | 23 February 2023 18:16:19 |
| Eccentricity: | 0.0447509 |
| inclination: | 63.4078° |
| perigee height: | 771 km |
| apogee height: | 1441 km |
| right ascension of ascending node: | 284.4655° |
| argument of perigee: | 0.2604° |
| revolutions per day: | 13.40871153 |
| mean anomaly at epoch: | 359.7396° |
| 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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