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 22148.45988777 .00000527 00000-0 22265-3 0 9999
2 00020 33.3391 171.9938 1664332 74.0767 303.6322 11.56209149312777
| Epoch (UTC): | 28 May 2022 11:02:14 |
| Eccentricity: | 0.1664332 |
| inclination: | 33.3391° |
| perigee height: | 508 km |
| apogee height: | 3258 km |
| right ascension of ascending node: | 171.9938° |
| argument of perigee: | 74.0767° |
| revolutions per day: | 11.56209149 |
| mean anomaly at epoch: | 303.6322° |
| orbit number at epoch: | 31277 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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