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 00012U 59001B 25082.84296383 .00001042 00000-0 58525-3 0 9993
2 00012 32.9125 11.3176 1651614 241.7482 100.6778 11.47644093479556
| Epoch (UTC): | 23 March 2025 20:13:52 |
| Eccentricity: | 0.1651614 |
| inclination: | 32.9125° |
| perigee height: | 553 km |
| apogee height: | 3295 km |
| right ascension of ascending node: | 11.3176° |
| argument of perigee: | 241.7482° |
| revolutions per day: | 11.47644093 |
| mean anomaly at epoch: | 100.6778° |
| orbit number at epoch: | 47955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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