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 23090.63125863 .00002530 00000-0 44837-3 0 9996
2 27939 98.2291 237.0762 0012847 26.5765 333.6104 14.68129589 43160
| Epoch (UTC): | 31 March 2023 15:09:00 |
| Eccentricity: | 0.0012847 |
| inclination: | 98.2291° |
| perigee height: | 658 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 237.0762° |
| argument of perigee: | 26.5765° |
| revolutions per day: | 14.68129589 |
| mean anomaly at epoch: | 333.6104° |
| orbit number at epoch: | 4316 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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