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 48515U 94074ES 23098.90031707 .25555384 26326-5 14218-1 0 9994
2 48515 97.7316 158.4658 0015403 270.9256 89.0267 16.19112572110334
| Epoch (UTC): | 08 April 2023 21:36:27 |
| Eccentricity: | 0.0015403 |
| inclination: | 97.7316° |
| perigee height: | 212 km |
| apogee height: | 232 km |
| right ascension of ascending node: | 158.4658° |
| argument of perigee: | 270.9256° |
| revolutions per day: | 16.19112572 |
| mean anomaly at epoch: | 89.0267° |
| orbit number at epoch: | 11033 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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