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 40908U 15049K 24340.13234823 .00018959 00000-0 60686-3 0 9990
2 40908 97.5192 350.7283 0012886 103.5572 256.7106 15.32367461509618
| Epoch (UTC): | 05 December 2024 03:10:34 |
| Eccentricity: | 0.0012886 |
| inclination: | 97.5192° |
| perigee height: | 460 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 350.7283° |
| argument of perigee: | 103.5572° |
| revolutions per day: | 15.32367461 |
| mean anomaly at epoch: | 256.7106° |
| orbit number at epoch: | 50961 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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