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 40538U 15015A 22270.86128113 0.00000000 00000-0 00000-0 0 08
2 40538 96.3977 329.6214 0053323 132.9789 227.2605 15.17782070 07
| Epoch (UTC): | 27 September 2022 20:40:14 |
| Eccentricity: | 0.0053323 |
| inclination: | 96.3977° |
| perigee height: | 476 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 329.6214° |
| argument of perigee: | 132.9789° |
| revolutions per day: | 15.17782070 |
| mean anomaly at epoch: | 227.2605° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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