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 27123U 01049BT 24357.55765800 .00002956 00000-0 50104-3 0 9991
2 27123 97.3175 357.0639 0040794 7.6280 352.5540 14.69361565226694
| Epoch (UTC): | 22 December 2024 13:23:01 |
| Eccentricity: | 0.0040794 |
| inclination: | 97.3175° |
| perigee height: | 634 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 357.0639° |
| argument of perigee: | 7.6280° |
| revolutions per day: | 14.69361565 |
| mean anomaly at epoch: | 352.5540° |
| orbit number at epoch: | 22669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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