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 28096U 03054B 20366.16478644 0.00000000 00000-0 00000-0 0 07
2 28096 63.6872 30.1845 0217190 223.7254 136.2746 13.40864869 03
| Epoch (UTC): | 31 December 2020 03:57:17 |
| Eccentricity: | 0.0217190 |
| inclination: | 63.6872° |
| perigee height: | 943 km |
| apogee height: | 1268 km |
| right ascension of ascending node: | 30.1845° |
| argument of perigee: | 223.7254° |
| revolutions per day: | 13.40864869 |
| mean anomaly at epoch: | 136.2746° |
| 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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