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 00011U 59001A 25140.34378645 .00001689 00000-0 88639-3 0 9990
2 00011 32.8674 131.2246 1448487 342.3531 13.1397 11.89781429488655
| Epoch (UTC): | 20 May 2025 08:15:03 |
| Eccentricity: | 0.1448487 |
| inclination: | 32.8674° |
| perigee height: | 553 km |
| apogee height: | 2901 km |
| right ascension of ascending node: | 131.2246° |
| argument of perigee: | 342.3531° |
| revolutions per day: | 11.89781429 |
| mean anomaly at epoch: | 13.1397° |
| orbit number at epoch: | 48865 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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