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 29043U 04035K 24279.86286284 .00011476 00000-0 82218-3 0 9991
2 29043 97.6247 298.9848 0003575 89.2596 270.9040 15.04539574 27859
| Epoch (UTC): | 05 October 2024 20:42:31 |
| Eccentricity: | 0.0003575 |
| inclination: | 97.6247° |
| perigee height: | 550 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 298.9848° |
| argument of perigee: | 89.2596° |
| revolutions per day: | 15.04539574 |
| mean anomaly at epoch: | 270.9040° |
| orbit number at epoch: | 2785 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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