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 26103.24314883 +.00000000 +00000-0 +48258-4 0 00000
2 14402 74.0422 99.0782 0027451 228.6856 131.1935 14.37382032 09
| Epoch (UTC): | 13 April 2026 05:50:08 |
| Eccentricity: | 0.0027451 |
| inclination: | 74.0422° |
| perigee height: | 748 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 99.0782° |
| argument of perigee: | 228.6856° |
| revolutions per day: | 14.37382032 |
| mean anomaly at epoch: | 131.1935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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