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 27403U 26105.98516947 +.00000000 +00000-0 +00000-0 0 00002
2 27403 7.5592 67.3386 0005818 221.3551 122.7837 0.99019990 06
| Epoch (UTC): | 15 April 2026 23:38:38 |
| Eccentricity: | 0.0005818 |
| inclination: | 7.5592° |
| perigee height: | 36116 km |
| apogee height: | 36166 km |
| right ascension of ascending node: | 67.3386° |
| argument of perigee: | 221.3551° |
| revolutions per day: | 0.99019990 |
| mean anomaly at epoch: | 122.7837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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