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 49256U 21086A 23027.84934313 .00008758 00000-0 52827-3 0 9997
2 49256 97.5594 136.8002 0021723 45.5383 69.3836 15.10782724 73596
| Epoch (UTC): | 27 January 2023 20:23:03 |
| Eccentricity: | 0.0021723 |
| inclination: | 97.5594° |
| perigee height: | 519 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 136.8002° |
| argument of perigee: | 45.5383° |
| revolutions per day: | 15.10782724 |
| mean anomaly at epoch: | 69.3836° |
| orbit number at epoch: | 7359 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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