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 23086.86756329 .00006191 00000-0 69992-3 0 9990
2 39444 97.6641 53.9525 0053857 178.8035 181.3319 14.85764080503566
| Epoch (UTC): | 27 March 2023 20:49:17 |
| Eccentricity: | 0.0053857 |
| inclination: | 97.6641° |
| perigee height: | 573 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 53.9525° |
| argument of perigee: | 178.8035° |
| revolutions per day: | 14.85764080 |
| mean anomaly at epoch: | 181.3319° |
| orbit number at epoch: | 50356 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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