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 29215U 02024F 24339.43045348 .00000807 00000-0 87805-3 0 9995
2 29215 98.8045 45.7712 0243852 279.8116 141.7683 13.63538582103984
| Epoch (UTC): | 04 December 2024 10:19:51 |
| Eccentricity: | 0.0243852 |
| inclination: | 98.8045° |
| perigee height: | 842 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 45.7712° |
| argument of perigee: | 279.8116° |
| revolutions per day: | 13.63538582 |
| mean anomaly at epoch: | 141.7683° |
| orbit number at epoch: | 10398 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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