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 27844U 03031E 23331.95483968 .00000757 00000-0 35561-3 0 9998
2 27844 98.6789 336.8462 0010079 17.5511 342.6013 14.22976569 59029
| Epoch (UTC): | 27 November 2023 22:54:58 |
| Eccentricity: | 0.0010079 |
| inclination: | 98.6789° |
| perigee height: | 808 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 336.8462° |
| argument of perigee: | 17.5511° |
| revolutions per day: | 14.22976569 |
| mean anomaly at epoch: | 342.6013° |
| orbit number at epoch: | 5902 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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