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 00020U 59007A 21109.88679313 .00000009 00000-0 10488-4 0 9995
2 00020 33.3407 170.2878 1666377 92.4041 286.7441 11.55804952266065
| Epoch (UTC): | 19 April 2021 21:16:58 |
| Eccentricity: | 0.1666377 |
| inclination: | 33.3407° |
| perigee height: | 508 km |
| apogee height: | 3262 km |
| right ascension of ascending node: | 170.2878° |
| argument of perigee: | 92.4041° |
| revolutions per day: | 11.55804952 |
| mean anomaly at epoch: | 286.7441° |
| orbit number at epoch: | 26606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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