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 22178.90659157 .00001615 00000-0 19739-3 0 9997
2 39444 97.6246 152.3379 0056696 0.3408 359.7836 14.83469664463079
| Epoch (UTC): | 27 June 2022 21:45:29 |
| Eccentricity: | 0.0056696 |
| inclination: | 97.6246° |
| perigee height: | 579 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 152.3379° |
| argument of perigee: | 0.3408° |
| revolutions per day: | 14.83469664 |
| mean anomaly at epoch: | 359.7836° |
| orbit number at epoch: | 46307 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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