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 27939U 03042A 22137.37072688 .00001072 00000-0 19867-3 0 9999
2 27939 98.1868 278.1079 0011758 309.5626 50.4551 14.67308618996489
| Epoch (UTC): | 17 May 2022 08:53:50 |
| Eccentricity: | 0.0011758 |
| inclination: | 98.1868° |
| perigee height: | 661 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 278.1079° |
| argument of perigee: | 309.5626° |
| revolutions per day: | 14.67308618 |
| mean anomaly at epoch: | 50.4551° |
| orbit number at epoch: | 99648 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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