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 11427U 26073.90444905 +.00000000 +00000-0 +12540-3 0 00006
2 11427 74.0141 262.6352 0019591 355.0778 5.0180 14.38846751 01
| Epoch (UTC): | 14 March 2026 21:42:24 |
| Eccentricity: | 0.0019591 |
| inclination: | 74.0141° |
| perigee height: | 748 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 262.6352° |
| argument of perigee: | 355.0778° |
| revolutions per day: | 14.38846751 |
| mean anomaly at epoch: | 5.0180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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