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 25137.70308767 .00001247 00000-0 50990-3 0 9999
2 00020 33.3412 249.5561 1643024 95.1737 283.7617 11.60647453438628
| Epoch (UTC): | 17 May 2025 16:52:26 |
| Eccentricity: | 0.1643024 |
| inclination: | 33.3412° |
| perigee height: | 508 km |
| apogee height: | 3216 km |
| right ascension of ascending node: | 249.5561° |
| argument of perigee: | 95.1737° |
| revolutions per day: | 11.60647453 |
| mean anomaly at epoch: | 283.7617° |
| orbit number at epoch: | 43862 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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