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 20U 59007A 23264.14915600 .00001117 00000-0 45912-3 0 9990
2 20 33.3406 256.1630 1656455 109.0276 269.6561 11.57824406368485
| Epoch (UTC): | 21 September 2023 03:34:47 |
| Eccentricity: | 0.1656455 |
| inclination: | 33.3406° |
| perigee height: | 508 km |
| apogee height: | 3242 km |
| right ascension of ascending node: | 256.1630° |
| argument of perigee: | 109.0276° |
| revolutions per day: | 11.57824406 |
| mean anomaly at epoch: | 269.6561° |
| orbit number at epoch: | 36848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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