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 44354U 19036R 23043.89354739 .05525980 -76587-5 75659-3 0 9997
2 44354 28.5071 258.5034 0024007 259.7469 100.0447 16.32955764202285
| Epoch (UTC): | 12 February 2023 21:26:42 |
| Eccentricity: | 0.0024007 |
| inclination: | 28.5071° |
| perigee height: | 169 km |
| apogee height: | 200 km |
| right ascension of ascending node: | 258.5034° |
| argument of perigee: | 259.7469° |
| revolutions per day: | 16.32955764 |
| mean anomaly at epoch: | 100.0447° |
| orbit number at epoch: | 20228 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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