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 is defined by the following mean orbital elements,
1 13001U 26065.52734816 +.00000000 +00000-0 +11571-2 0 00000
2 13001 82.9530 79.2430 0022888 218.5869 311.8669 12.08947325 01
| Epoch (UTC): | 06 March 2026 12:39:22 |
| Eccentricity: | 0.0022888 |
| inclination: | 82.9530° |
| perigee height: | 1623 km |
| apogee height: | 1659 km |
| right ascension of ascending node: | 79.2430° |
| argument of perigee: | 218.5869° |
| revolutions per day: | 12.08947325 |
| mean anomaly at epoch: | 311.8669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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