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 40071U 14037C 24357.85938350 .00004545 00000-0 51632-3 0 9997
2 40071 98.3352 279.1271 0006348 225.8939 134.1753 14.86805095565570
| Epoch (UTC): | 22 December 2024 20:37:30 |
| Eccentricity: | 0.0006348 |
| inclination: | 98.3352° |
| perigee height: | 603 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 279.1271° |
| argument of perigee: | 225.8939° |
| revolutions per day: | 14.86805095 |
| mean anomaly at epoch: | 134.1753° |
| orbit number at epoch: | 56557 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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