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 23089.48437133 .00000838 00000-0 39360-3 0 9990
2 27844 98.6810 97.8887 0009751 1.1323 358.9875 14.22703350 24578
| Epoch (UTC): | 30 March 2023 11:37:29 |
| Eccentricity: | 0.0009751 |
| inclination: | 98.6810° |
| perigee height: | 809 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 97.8887° |
| argument of perigee: | 1.1323° |
| revolutions per day: | 14.22703350 |
| mean anomaly at epoch: | 358.9875° |
| orbit number at epoch: | 2457 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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