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 39446U 13066AG 23087.86900609 .00005063 00000-0 63073-3 0 9996
2 39446 97.7263 45.5384 0064573 240.9179 118.5558 14.81421830503124
| Epoch (UTC): | 28 March 2023 20:51:22 |
| Eccentricity: | 0.0064573 |
| inclination: | 97.7263° |
| perigee height: | 579 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 45.5384° |
| argument of perigee: | 240.9179° |
| revolutions per day: | 14.81421830 |
| mean anomaly at epoch: | 118.5558° |
| orbit number at epoch: | 50312 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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