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 39444U 13066AE 23089.15735059 .00006940 00000-0 78303-3 0 9990
2 39444 97.6636 56.1578 0054097 171.2778 188.9391 14.85794657504490
| Epoch (UTC): | 30 March 2023 03:46:35 |
| Eccentricity: | 0.0054097 |
| inclination: | 97.6636° |
| perigee height: | 573 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 56.1578° |
| argument of perigee: | 171.2778° |
| revolutions per day: | 14.85794657 |
| mean anomaly at epoch: | 188.9391° |
| orbit number at epoch: | 50449 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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