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 26486U 00051D 25133.06333196 -.00000024 00000-0 00000-0 0 9994
2 26486 63.1925 265.2485 6954456 278.3465 339.9651 1.45766109131404
| Epoch (UTC): | 13 May 2025 01:31:11 |
| Eccentricity: | 0.6954456 |
| inclination: | 63.1925° |
| perigee height: | 3628 km |
| apogee height: | 49329 km |
| right ascension of ascending node: | 265.2485° |
| argument of perigee: | 278.3465° |
| revolutions per day: | 1.45766109 |
| mean anomaly at epoch: | 339.9651° |
| orbit number at epoch: | 13140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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