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 10061U 26103.87123858 +.00000000 +00000-0 +00000-0 0 00005
2 10061 6.5732 293.9153 0013653 52.7011 157.1765 0.99401648 02
| Epoch (UTC): | 13 April 2026 20:54:35 |
| Eccentricity: | 0.0013653 |
| inclination: | 6.5732° |
| perigee height: | 35974 km |
| apogee height: | 36090 km |
| right ascension of ascending node: | 293.9153° |
| argument of perigee: | 52.7011° |
| revolutions per day: | 0.99401648 |
| mean anomaly at epoch: | 157.1765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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