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 22179.71736642 .00000535 00000-0 10337-3 0 9996
2 27939 98.1927 320.4352 0013202 167.0618 193.0933 14.67373265 2693
| Epoch (UTC): | 28 June 2022 17:13:00 |
| Eccentricity: | 0.0013202 |
| inclination: | 98.1927° |
| perigee height: | 660 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 320.4352° |
| argument of perigee: | 167.0618° |
| revolutions per day: | 14.67373265 |
| mean anomaly at epoch: | 193.0933° |
| orbit number at epoch: | 269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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