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 22178.56745104 .00005034 00000-0 23761-3 0 9995
2 40907 97.4907 181.8879 0012120 326.8587 152.5104 15.19842622374502
| Epoch (UTC): | 27 June 2022 13:37:07 |
| Eccentricity: | 0.0012120 |
| inclination: | 97.4907° |
| perigee height: | 498 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 181.8879° |
| argument of perigee: | 326.8587° |
| revolutions per day: | 15.19842622 |
| mean anomaly at epoch: | 152.5104° |
| orbit number at epoch: | 37450 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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