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 36122U 09072B 25143.44221858 -.00000016 00000-0 74034-4 0 9991
2 36122 100.3482 99.5810 0008043 47.9859 312.1937 13.16424527741725
| Epoch (UTC): | 23 May 2025 10:36:47 |
| Eccentricity: | 0.0008043 |
| inclination: | 100.3482° |
| perigee height: | 1192 km |
| apogee height: | 1204 km |
| right ascension of ascending node: | 99.5810° |
| argument of perigee: | 47.9859° |
| revolutions per day: | 13.16424527 |
| mean anomaly at epoch: | 312.1937° |
| orbit number at epoch: | 74172 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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