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 40889U 15045A 25190.67107840 .00000082 00000-0 00000-0 0 9994
2 40889 55.0586 231.0656 0002760 9.2239 350.8804 1.70473773 61175
| Epoch (UTC): | 09 July 2025 16:06:21 |
| Eccentricity: | 0.0002760 |
| inclination: | 55.0586° |
| perigee height: | 23214 km |
| apogee height: | 23230 km |
| right ascension of ascending node: | 231.0656° |
| argument of perigee: | 9.2239° |
| revolutions per day: | 1.70473773 |
| mean anomaly at epoch: | 350.8804° |
| orbit number at epoch: | 6117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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