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 27844U 03031E 24357.81937878 .00000773 00000-0 35763-3 0 9998
2 27844 98.6778 2.2876 0009033 322.7675 37.2876 14.23714342114622
| Epoch (UTC): | 22 December 2024 19:39:54 |
| Eccentricity: | 0.0009033 |
| inclination: | 98.6778° |
| perigee height: | 806 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 2.2876° |
| argument of perigee: | 322.7675° |
| revolutions per day: | 14.23714342 |
| mean anomaly at epoch: | 37.2876° |
| orbit number at epoch: | 11462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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