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 29U 60002B 24287.82172726 .00002780 00000-0 41811-3 0 9992
2 29 48.3780 46.9594 0022598 159.2105 200.9732 14.77011495451809
| Epoch (UTC): | 13 October 2024 19:43:17 |
| Eccentricity: | 0.0022598 |
| inclination: | 48.3780° |
| perigee height: | 623 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 46.9594° |
| argument of perigee: | 159.2105° |
| revolutions per day: | 14.77011495 |
| mean anomaly at epoch: | 200.9732° |
| orbit number at epoch: | 45180 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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