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 63157U 26144.71344794 +.00000000 +00000-0 +00000-0 0 00001
2 63157 0.2779 84.9730 0005613 295.0455 213.5325 1.00274561 02
| Epoch (UTC): | 24 May 2026 17:07:21 |
| Eccentricity: | 0.0005613 |
| inclination: | 0.2779° |
| perigee height: | 35762 km |
| apogee height: | 35809 km |
| right ascension of ascending node: | 84.9730° |
| argument of perigee: | 295.0455° |
| revolutions per day: | 1.00274561 |
| mean anomaly at epoch: | 213.5325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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