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 14402U 26106.23590889 +.00000000 +00000-0 +21037-4 0 00000
2 14402 74.0427 93.5742 0027390 222.6367 137.2662 14.37382206 09
| Epoch (UTC): | 16 April 2026 05:39:42 |
| Eccentricity: | 0.0027390 |
| inclination: | 74.0427° |
| perigee height: | 748 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 93.5742° |
| argument of perigee: | 222.6367° |
| revolutions per day: | 14.37382206 |
| mean anomaly at epoch: | 137.2662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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