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 40911U 15049N 22178.80099333 .00005011 00000-0 23731-3 0 9995
2 40911 97.4896 182.7173 0011927 327.5354 207.3669 15.19731964374427
| Epoch (UTC): | 27 June 2022 19:13:25 |
| Eccentricity: | 0.0011927 |
| inclination: | 97.4896° |
| perigee height: | 498 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 182.7173° |
| argument of perigee: | 327.5354° |
| revolutions per day: | 15.19731964 |
| mean anomaly at epoch: | 207.3669° |
| orbit number at epoch: | 37442 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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