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 25724U 99023A 23059.81925592 0.00000000 00000-0 00000-0 0 06
2 25724 28.2484 344.3917 2136344 188.0713 171.9605 9.37488881 07
| Epoch (UTC): | 28 February 2023 19:39:43 |
| Eccentricity: | 0.2136344 |
| inclination: | 28.2484° |
| perigee height: | 1093 km |
| apogee height: | 5152 km |
| right ascension of ascending node: | 344.3917° |
| argument of perigee: | 188.0713° |
| revolutions per day: | 9.37488881 |
| mean anomaly at epoch: | 171.9605° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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