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 22179.58596902 .00002530 00000-0 13550-3 0 9992
2 40908 97.5154 180.0579 0014869 344.9539 133.3019 15.15858720374173
| Epoch (UTC): | 28 June 2022 14:03:47 |
| Eccentricity: | 0.0014869 |
| inclination: | 97.5154° |
| perigee height: | 508 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 180.0579° |
| argument of perigee: | 344.9539° |
| revolutions per day: | 15.15858720 |
| mean anomaly at epoch: | 133.3019° |
| orbit number at epoch: | 37417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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