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 27386U 02009A 22229.48148542 .00000077 00000-0 39077-4 0 9994
2 27386 98.1881 207.7411 0001414 86.2853 25.2969 14.38145403 72305
| Epoch (UTC): | 17 August 2022 11:33:20 |
| Eccentricity: | 0.0001414 |
| inclination: | 98.1881° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 207.7411° |
| argument of perigee: | 86.2853° |
| revolutions per day: | 14.38145403 |
| mean anomaly at epoch: | 25.2969° |
| orbit number at epoch: | 7230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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