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 23657U 95046A 25201.50857462 .00001357 00000-0 12729-3 0 9994
2 23657 82.5250 357.7001 0019149 0.3071 359.8157 14.93137446616772
| Epoch (UTC): | 20 July 2025 12:12:20 |
| Eccentricity: | 0.0019149 |
| inclination: | 82.5250° |
| perigee height: | 575 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 357.7001° |
| argument of perigee: | 0.3071° |
| revolutions per day: | 14.93137446 |
| mean anomaly at epoch: | 359.8157° |
| orbit number at epoch: | 61677 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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