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 is defined by the following mean orbital elements,
1 879U 64054A 20233.75378097 -.00000811 +00000-0 +00000-0 0 9990
2 879 054.9668 307.2269 9131889 205.8880 032.8586 00.40281857021812
| Epoch (UTC): | 20 August 2020 18:05:26 |
| Eccentricity: | 0.9131889 |
| inclination: | 54.9668° |
| perigee height: | 345 km |
| apogee height: | 141788 km |
| right ascension of ascending node: | 307.2269° |
| argument of perigee: | 205.8880° |
| revolutions per day: | 0.40281857 |
| mean anomaly at epoch: | 32.8586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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