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 15945U 85069B 24357.71985574 .00001060 00000-0 11909-3 0 9999
2 15945 82.5273 80.3400 0018348 212.3016 147.7079 14.85740045107198
| Epoch (UTC): | 22 December 2024 17:16:35 |
| Eccentricity: | 0.0018348 |
| inclination: | 82.5273° |
| perigee height: | 598 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 80.3400° |
| argument of perigee: | 212.3016° |
| revolutions per day: | 14.85740045 |
| mean anomaly at epoch: | 147.7079° |
| orbit number at epoch: | 10719 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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