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 24282.85861344 0.00000600 00000-0 52531-3 0 04
2 28541 63.4005 207.4278 0498000 2.0202 357.9798 13.40505250 00
| Epoch (UTC): | 08 October 2024 20:36:24 |
| Eccentricity: | 0.0498000 |
| inclination: | 63.4005° |
| perigee height: | 734 km |
| apogee height: | 1480 km |
| right ascension of ascending node: | 207.4278° |
| argument of perigee: | 2.0202° |
| revolutions per day: | 13.40505250 |
| mean anomaly at epoch: | 357.9798° |
| 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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