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 20253U 89077A 23273.54667653 -.00000376 00000-0 00000+0 0 9998
2 20253 12.7172 357.1623 0003840 178.1637 156.2987 1.00269301250668
| Epoch (UTC): | 30 September 2023 13:07:12 |
| Eccentricity: | 0.0003840 |
| inclination: | 12.7172° |
| perigee height: | 35771 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 357.1623° |
| argument of perigee: | 178.1637° |
| revolutions per day: | 1.00269301 |
| mean anomaly at epoch: | 156.2987° |
| orbit number at epoch: | 25066 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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