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 40544U 15017A 24337.26533323 -.00000061 00000-0 00000+0 0 9994
2 40544 56.9149 356.8985 0006113 263.8341 96.1481 1.70476094 60288
| Epoch (UTC): | 02 December 2024 06:22:04 |
| Eccentricity: | 0.0006113 |
| inclination: | 56.9149° |
| perigee height: | 23203 km |
| apogee height: | 23240 km |
| right ascension of ascending node: | 356.8985° |
| argument of perigee: | 263.8341° |
| revolutions per day: | 1.70476094 |
| mean anomaly at epoch: | 96.1481° |
| orbit number at epoch: | 6028 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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