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 29870U 99025FQ 24357.88973924 .00000250 00000-0 10741-3 0 9995
2 29870 98.4137 334.2261 0120941 158.1471 232.8963 14.28759648935267
| Epoch (UTC): | 22 December 2024 21:21:13 |
| Eccentricity: | 0.0120941 |
| inclination: | 98.4137° |
| perigee height: | 709 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 334.2261° |
| argument of perigee: | 158.1471° |
| revolutions per day: | 14.28759648 |
| mean anomaly at epoch: | 232.8963° |
| orbit number at epoch: | 93526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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