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 02861U 26132.43546102 +.00000000 +00000-0 +64394-3 0 00008
2 02861 89.9760 314.1169 0072693 136.6348 224.0238 8.36661302 07
| Epoch (UTC): | 12 May 2026 10:27:03 |
| Eccentricity: | 0.0072693 |
| inclination: | 89.9760° |
| perigee height: | 3797 km |
| apogee height: | 3946 km |
| right ascension of ascending node: | 314.1169° |
| argument of perigee: | 136.6348° |
| revolutions per day: | 8.36661302 |
| mean anomaly at epoch: | 224.0238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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