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 23341.44729455 .00000425 00000-0 20808-3 0 9997
2 27844 98.6789 346.2009 0009521 350.2156 9.8835 14.22991271 60374
| Epoch (UTC): | 07 December 2023 10:44:06 |
| Eccentricity: | 0.0009521 |
| inclination: | 98.6789° |
| perigee height: | 808 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 346.2009° |
| argument of perigee: | 350.2156° |
| revolutions per day: | 14.22991271 |
| mean anomaly at epoch: | 9.8835° |
| orbit number at epoch: | 6037 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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