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 21108.84982092 .00000004 00000-0 89568-5 0 9992
2 00020 33.3407 173.9829 1666374 86.9027 292.0061 11.55804836265945
| Epoch (UTC): | 18 April 2021 20:23:44 |
| Eccentricity: | 0.1666374 |
| inclination: | 33.3407° |
| perigee height: | 508 km |
| apogee height: | 3262 km |
| right ascension of ascending node: | 173.9829° |
| argument of perigee: | 86.9027° |
| revolutions per day: | 11.55804836 |
| mean anomaly at epoch: | 292.0061° |
| orbit number at epoch: | 26594 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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