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 22178.59601076 .00002742 00000-0 14654-3 0 9992
2 40908 97.5157 179.0779 0014998 348.8172 130.5910 15.15855046374026
| Epoch (UTC): | 27 June 2022 14:18:15 |
| Eccentricity: | 0.0014998 |
| inclination: | 97.5157° |
| perigee height: | 508 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 179.0779° |
| argument of perigee: | 348.8172° |
| revolutions per day: | 15.15855046 |
| mean anomaly at epoch: | 130.5910° |
| orbit number at epoch: | 37402 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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