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 24262.44382632 .00001116 00000-0 51030-3 0 9991
2 27844 98.6802 268.1943 0008705 229.3034 130.7389 14.23472130101051
| Epoch (UTC): | 18 September 2024 10:39:06 |
| Eccentricity: | 0.0008705 |
| inclination: | 98.6802° |
| perigee height: | 807 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 268.1943° |
| argument of perigee: | 229.3034° |
| revolutions per day: | 14.23472130 |
| mean anomaly at epoch: | 130.7389° |
| orbit number at epoch: | 10105 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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