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 23092.01619082 .00000774 00000-0 36504-3 0 9994
2 27844 98.6808 100.3837 0009597 353.7899 6.3158 14.22707127 24936
| Epoch (UTC): | 02 April 2023 00:23:18 |
| Eccentricity: | 0.0009597 |
| inclination: | 98.6808° |
| perigee height: | 809 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 100.3837° |
| argument of perigee: | 353.7899° |
| revolutions per day: | 14.22707127 |
| mean anomaly at epoch: | 6.3158° |
| orbit number at epoch: | 2493 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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