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 23085.75695693 .00000818 00000-0 38453-3 0 9993
2 27844 98.6811 94.2155 0009977 11.8584 348.2827 14.22696938 24016
| Epoch (UTC): | 26 March 2023 18:10:01 |
| Eccentricity: | 0.0009977 |
| inclination: | 98.6811° |
| perigee height: | 809 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 94.2155° |
| argument of perigee: | 11.8584° |
| revolutions per day: | 14.22696938 |
| mean anomaly at epoch: | 348.2827° |
| orbit number at epoch: | 2401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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