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 08459U 75112B 25189.47392510 .00000158 00000-0 60900-4 0 9991
2 08459 74.0612 108.1024 0016824 260.4352 99.4901 14.38032392596767
| Epoch (UTC): | 08 July 2025 11:22:27 |
| Eccentricity: | 0.0016824 |
| inclination: | 74.0612° |
| perigee height: | 753 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 108.1024° |
| argument of perigee: | 260.4352° |
| revolutions per day: | 14.38032392 |
| mean anomaly at epoch: | 99.4901° |
| orbit number at epoch: | 59676 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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