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 40491U 95015CE 24356.55762656 .00014988 00000-0 40631-2 0 9996
2 40491 98.5917 29.9195 0023322 343.3137 16.7285 14.47563502511441
| Epoch (UTC): | 21 December 2024 13:22:58 |
| Eccentricity: | 0.0023322 |
| inclination: | 98.5917° |
| perigee height: | 717 km |
| apogee height: | 750 km |
| right ascension of ascending node: | 29.9195° |
| argument of perigee: | 343.3137° |
| revolutions per day: | 14.47563502 |
| mean anomaly at epoch: | 16.7285° |
| orbit number at epoch: | 51144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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