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 39307U 94029AES 25321.81189777 .00051134 00000-0 23909-2 0 9996
2 39307 81.9438 92.6726 0094921 121.0675 239.9916 15.15553542751363
| Epoch (UTC): | 17 November 2025 19:29:07 |
| Eccentricity: | 0.0094921 |
| inclination: | 81.9438° |
| perigee height: | 454 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 92.6726° |
| argument of perigee: | 121.0675° |
| revolutions per day: | 15.15553542 |
| mean anomaly at epoch: | 239.9916° |
| orbit number at epoch: | 75136 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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