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 23090.76756740 .00002527 00000-0 44776-3 0 9992
2 27939 98.2290 237.2131 0012835 26.1761 334.0094 14.68130324 43184
| Epoch (UTC): | 31 March 2023 18:25:17 |
| Eccentricity: | 0.0012835 |
| inclination: | 98.2290° |
| perigee height: | 658 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 237.2131° |
| argument of perigee: | 26.1761° |
| revolutions per day: | 14.68130324 |
| mean anomaly at epoch: | 334.0094° |
| orbit number at epoch: | 4318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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