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 27711U 03012A 23088.74563458 -.00000267 00000-0 00000+0 0 9992
2 27711 10.5536 38.3975 0100573 350.7889 218.2954 1.00273551 19859
| Epoch (UTC): | 29 March 2023 17:53:42 |
| Eccentricity: | 0.0100573 |
| inclination: | 10.5536° |
| perigee height: | 35361 km |
| apogee height: | 36210 km |
| right ascension of ascending node: | 38.3975° |
| argument of perigee: | 350.7889° |
| revolutions per day: | 1.00273551 |
| mean anomaly at epoch: | 218.2954° |
| orbit number at epoch: | 1985 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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