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 21063.86976652 .00000308 00000-0 36073-4 0 9994
2 28647 56.9965 261.2245 0119285 252.6601 106.1360 15.06276858 99192
| Epoch (UTC): | 04 March 2021 20:52:27 |
| Eccentricity: | 0.0119285 |
| inclination: | 56.9965° |
| perigee height: | 465 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 261.2245° |
| argument of perigee: | 252.6601° |
| revolutions per day: | 15.06276858 |
| mean anomaly at epoch: | 106.1360° |
| orbit number at epoch: | 9919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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