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 35756U 09044B 25341.88437385 -.00000142 00000-0 00000-0 0 9992
2 35756 0.8278 270.3919 0001897 350.8448 290.1546 1.00271372 59645
| Epoch (UTC): | 07 December 2025 21:13:29 |
| Eccentricity: | 0.0001897 |
| inclination: | 0.8278° |
| perigee height: | 35778 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 270.3919° |
| argument of perigee: | 350.8448° |
| revolutions per day: | 1.00271372 |
| mean anomaly at epoch: | 290.1546° |
| orbit number at epoch: | 5964 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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