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 40315U 14075A 22274.10990942 .00000060 00000-0 00000+0 0 9996
2 40315 63.6773 237.4701 0019251 212.1601 170.8966 2.13101441 60989
| Epoch (UTC): | 01 October 2022 02:38:16 |
| Eccentricity: | 0.0019251 |
| inclination: | 63.6773° |
| perigee height: | 19080 km |
| apogee height: | 19179 km |
| right ascension of ascending node: | 237.4701° |
| argument of perigee: | 212.1601° |
| revolutions per day: | 2.13101441 |
| mean anomaly at epoch: | 170.8966° |
| orbit number at epoch: | 6098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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