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 23343.84364590 .00001032 00000-0 18444-3 0 9993
2 27939 98.2651 132.4687 0011331 304.8455 192.8447 14.69070248 80321
| Epoch (UTC): | 09 December 2023 20:14:51 |
| Eccentricity: | 0.0011331 |
| inclination: | 98.2651° |
| perigee height: | 656 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 132.4687° |
| argument of perigee: | 304.8455° |
| revolutions per day: | 14.69070248 |
| mean anomaly at epoch: | 192.8447° |
| orbit number at epoch: | 8032 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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