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 22181.21754242 .00000402 00000-0 79806-4 0 9990
2 27939 98.1933 321.9354 0013387 162.6501 197.5161 14.67373941 2912
| Epoch (UTC): | 30 June 2022 05:13:15 |
| Eccentricity: | 0.0013387 |
| inclination: | 98.1933° |
| perigee height: | 660 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 321.9354° |
| argument of perigee: | 162.6501° |
| revolutions per day: | 14.67373941 |
| mean anomaly at epoch: | 197.5161° |
| orbit number at epoch: | 291 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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