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 39440U 13066AA 23090.10359764 .00006944 00000-0 90704-3 0 9991
2 39440 97.7643 41.4735 0074358 281.6186 77.6687 14.78848759503810
| Epoch (UTC): | 31 March 2023 02:29:10 |
| Eccentricity: | 0.0074358 |
| inclination: | 97.7643° |
| perigee height: | 581 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 41.4735° |
| argument of perigee: | 281.6186° |
| revolutions per day: | 14.78848759 |
| mean anomaly at epoch: | 77.6687° |
| orbit number at epoch: | 50381 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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