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 00116U 61015A 21101.76631112 -.00000037 00000-0 30497-4 0 9991
2 00116 66.8102 198.9390 0073384 164.8999 195.4295 13.91787426 33327
| Epoch (UTC): | 11 April 2021 18:23:29 |
| Eccentricity: | 0.0073384 |
| inclination: | 66.8102° |
| perigee height: | 869 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 198.9390° |
| argument of perigee: | 164.8999° |
| revolutions per day: | 13.91787426 |
| mean anomaly at epoch: | 195.4295° |
| orbit number at epoch: | 3332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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