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 26533U 79104P 21343.95594557 -.00000064 00000-0 00000+0 0 9992
2 26533 16.0602 80.7079 5793704 140.2452 2.5379 3.66991107292124
| Epoch (UTC): | 09 December 2021 22:56:33 |
| Eccentricity: | 0.5793704 |
| inclination: | 16.0602° |
| perigee height: | 1090 km |
| apogee height: | 21662 km |
| right ascension of ascending node: | 80.7079° |
| argument of perigee: | 140.2452° |
| revolutions per day: | 3.66991107 |
| mean anomaly at epoch: | 2.5379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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