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 23038.93757262 .00004056 00000-0 16709-2 0 9990
2 00020 33.3480 340.8941 1660070 350.7473 6.5770 11.56698498342352
| Epoch (UTC): | 07 February 2023 22:30:06 |
| Eccentricity: | 0.1660070 |
| inclination: | 33.3480° |
| perigee height: | 510 km |
| apogee height: | 3252 km |
| right ascension of ascending node: | 340.8941° |
| argument of perigee: | 350.7473° |
| revolutions per day: | 11.56698498 |
| mean anomaly at epoch: | 6.5770° |
| orbit number at epoch: | 34235 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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