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 40907U 15049J 22178.77505392 .00004957 00000-0 23403-3 0 9997
2 40907 97.4909 182.0942 0011937 325.9135 208.6171 15.19844231374530
| Epoch (UTC): | 27 June 2022 18:36:04 |
| Eccentricity: | 0.0011937 |
| inclination: | 97.4909° |
| perigee height: | 498 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 182.0942° |
| argument of perigee: | 325.9135° |
| revolutions per day: | 15.19844231 |
| mean anomaly at epoch: | 208.6171° |
| orbit number at epoch: | 37453 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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