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 23340.46289582 .00000527 00000-0 25339-3 0 9997
2 27844 98.6790 345.2308 0009577 353.1085 6.9960 14.22990495 60230
| Epoch (UTC): | 06 December 2023 11:06:34 |
| Eccentricity: | 0.0009577 |
| inclination: | 98.6790° |
| perigee height: | 808 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 345.2308° |
| argument of perigee: | 353.1085° |
| revolutions per day: | 14.22990495 |
| mean anomaly at epoch: | 6.9960° |
| orbit number at epoch: | 6023 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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