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 24349.22294006 0.00000100 00000-0 87254-4 0 05
2 28537 63.4045 36.2521 0495301 2.9221 357.0779 13.41080750 03
| Epoch (UTC): | 14 December 2024 05:21:02 |
| Eccentricity: | 0.0495301 |
| inclination: | 63.4045° |
| perigee height: | 734 km |
| apogee height: | 1476 km |
| right ascension of ascending node: | 36.2521° |
| argument of perigee: | 2.9221° |
| revolutions per day: | 13.41080750 |
| mean anomaly at epoch: | 357.0779° |
| 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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