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 44879U 19093A 23150.51227151 .00002445 00000-0 29937-3 0 9997
2 44879 97.8660 230.2356 0015497 129.0007 231.2589 14.84022716186231
| Epoch (UTC): | 30 May 2023 12:17:40 |
| Eccentricity: | 0.0015497 |
| inclination: | 97.8660° |
| perigee height: | 606 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 230.2356° |
| argument of perigee: | 129.0007° |
| revolutions per day: | 14.84022716 |
| mean anomaly at epoch: | 231.2589° |
| orbit number at epoch: | 18623 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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