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 21107.46713046 -.00000023 00000-0 -18363-5 0 9998
2 00020 33.3407 178.9097 1666363 79.5675 298.7684 11.55804526265784
| Epoch (UTC): | 17 April 2021 11:12:40 |
| Eccentricity: | 0.1666363 |
| inclination: | 33.3407° |
| perigee height: | 508 km |
| apogee height: | 3262 km |
| right ascension of ascending node: | 178.9097° |
| argument of perigee: | 79.5675° |
| revolutions per day: | 11.55804526 |
| mean anomaly at epoch: | 298.7684° |
| orbit number at epoch: | 26578 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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