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 26474U 00047B 23159.54129983 .00003015 00000-0 25345-3 0 9996
2 26474 67.9941 322.7258 0047573 81.9913 278.6625 14.98867229241848
| Epoch (UTC): | 08 June 2023 12:59:28 |
| Eccentricity: | 0.0047573 |
| inclination: | 67.9941° |
| perigee height: | 537 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 322.7258° |
| argument of perigee: | 81.9913° |
| revolutions per day: | 14.98867229 |
| mean anomaly at epoch: | 278.6625° |
| orbit number at epoch: | 24184 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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