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 27640U 03001A 24284.54137569 .00000724 00000-0 36322-3 0 9995
2 27640 98.7162 289.9371 0014095 178.4350 181.6873 14.19592494126966
| Epoch (UTC): | 10 October 2024 12:59:34 |
| Eccentricity: | 0.0014095 |
| inclination: | 98.7162° |
| perigee height: | 816 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 289.9371° |
| argument of perigee: | 178.4350° |
| revolutions per day: | 14.19592494 |
| mean anomaly at epoch: | 181.6873° |
| orbit number at epoch: | 12696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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