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 31293U 99025BPB 24357.26501496 .00000352 00000-0 13942-3 0 9999
2 31293 98.4334 9.7715 0126249 215.7013 143.5680 14.30565942601613
| Epoch (UTC): | 22 December 2024 06:21:37 |
| Eccentricity: | 0.0126249 |
| inclination: | 98.4334° |
| perigee height: | 699 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 9.7715° |
| argument of perigee: | 215.7013° |
| revolutions per day: | 14.30565942 |
| mean anomaly at epoch: | 143.5680° |
| orbit number at epoch: | 60161 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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