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 28647U 05016B 21062.80789912 .00000348 00000-0 38329-4 0 9998
2 28647 56.9966 265.5447 0119359 250.6600 108.1501 15.06275648 99031
| Epoch (UTC): | 03 March 2021 19:23:22 |
| Eccentricity: | 0.0119359 |
| inclination: | 56.9966° |
| perigee height: | 465 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 265.5447° |
| argument of perigee: | 250.6600° |
| revolutions per day: | 15.06275648 |
| mean anomaly at epoch: | 108.1501° |
| orbit number at epoch: | 9903 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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