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 40910U 15049M 22179.57074811 .00007464 00000-0 31806-3 0 9999
2 40910 97.4720 186.5697 0011165 301.7992 175.1972 15.23192843374871
| Epoch (UTC): | 28 June 2022 13:41:52 |
| Eccentricity: | 0.0011165 |
| inclination: | 97.4720° |
| perigee height: | 488 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 186.5697° |
| argument of perigee: | 301.7992° |
| revolutions per day: | 15.23192843 |
| mean anomaly at epoch: | 175.1972° |
| orbit number at epoch: | 37487 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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