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 27387U 02009B 22183.88188303 .00000014 00000-0 20317-4 0 9995
2 27387 98.7130 152.1495 0033543 74.1539 286.3339 14.36073332 65828
| Epoch (UTC): | 02 July 2022 21:09:54 |
| Eccentricity: | 0.0033543 |
| inclination: | 98.7130° |
| perigee height: | 747 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 152.1495° |
| argument of perigee: | 74.1539° |
| revolutions per day: | 14.36073332 |
| mean anomaly at epoch: | 286.3339° |
| orbit number at epoch: | 6582 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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