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 08344U 75094B 25196.85501954 .00000140 00000-0 52340-4 0 9997
2 08344 74.0558 85.9276 0022102 325.2084 34.7625 14.40422166609932
| Epoch (UTC): | 15 July 2025 20:31:13 |
| Eccentricity: | 0.0022102 |
| inclination: | 74.0558° |
| perigee height: | 741 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 85.9276° |
| argument of perigee: | 325.2084° |
| revolutions per day: | 14.40422166 |
| mean anomaly at epoch: | 34.7625° |
| orbit number at epoch: | 60993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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