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 26931U 01043C 23089.49688522 .00000600 00000-0 25995-3 0 9994
2 26931 67.0526 40.0002 0007051 282.4393 77.5919 14.30871319122481
| Epoch (UTC): | 30 March 2023 11:55:30 |
| Eccentricity: | 0.0007051 |
| inclination: | 67.0526° |
| perigee height: | 784 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 40.0002° |
| argument of perigee: | 282.4393° |
| revolutions per day: | 14.30871319 |
| mean anomaly at epoch: | 77.5919° |
| orbit number at epoch: | 12248 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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