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 44881U 19093C 23081.76414145 .00001631 00000-0 21042-3 0 9996
2 44881 97.8657 161.6859 0014903 5.2144 354.9205 14.82290562175996
| Epoch (UTC): | 22 March 2023 18:20:21 |
| Eccentricity: | 0.0014903 |
| inclination: | 97.8657° |
| perigee height: | 611 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 161.6859° |
| argument of perigee: | 5.2144° |
| revolutions per day: | 14.82290562 |
| mean anomaly at epoch: | 354.9205° |
| orbit number at epoch: | 17599 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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