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 23078.85291541 .00006011 00000-0 68224-3 0 9998
2 39444 97.6619 46.2332 0053076 205.4678 154.3921 14.85648065502376
| Epoch (UTC): | 19 March 2023 20:28:11 |
| Eccentricity: | 0.0053076 |
| inclination: | 97.6619° |
| perigee height: | 574 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 46.2332° |
| argument of perigee: | 205.4678° |
| revolutions per day: | 14.85648065 |
| mean anomaly at epoch: | 154.3921° |
| orbit number at epoch: | 50237 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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