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 25634U 99008A 23031.51738896 .00000083 00000-0 58937-4 0 9999
2 25634 98.3928 38.8524 0010624 23.5192 336.6469 14.19480182239881
| Epoch (UTC): | 31 January 2023 12:25:02 |
| Eccentricity: | 0.0010624 |
| inclination: | 98.3928° |
| perigee height: | 819 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 38.8524° |
| argument of perigee: | 23.5192° |
| revolutions per day: | 14.19480182 |
| mean anomaly at epoch: | 336.6469° |
| orbit number at epoch: | 23988 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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