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 26106.65350337 +.00000000 +00000-0 +17872-4 0 00000
2 14402 74.0427 92.8061 0027372 221.8159 138.0904 14.37382202 09
| Epoch (UTC): | 16 April 2026 15:41:02 |
| Eccentricity: | 0.0027372 |
| inclination: | 74.0427° |
| perigee height: | 748 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 92.8061° |
| argument of perigee: | 221.8159° |
| revolutions per day: | 14.37382202 |
| mean anomaly at epoch: | 138.0904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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