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 44909U 19096E 23086.13196056 .00000036 00000-0 99803-4 0 9993
2 44909 82.5233 42.4597 0217979 19.1163 341.7959 12.79719400151711
| Epoch (UTC): | 27 March 2023 03:10:01 |
| Eccentricity: | 0.0217979 |
| inclination: | 82.5233° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 42.4597° |
| argument of perigee: | 19.1163° |
| revolutions per day: | 12.79719400 |
| mean anomaly at epoch: | 341.7959° |
| orbit number at epoch: | 15171 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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