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 40014U 26101.53635587 +.00000000 +00000-0 +17913-3 0 00008
2 40014 98.0401 190.2326 0029279 50.4260 309.9550 15.14942097 05
| Epoch (UTC): | 11 April 2026 12:52:21 |
| Eccentricity: | 0.0029279 |
| inclination: | 98.0401° |
| perigee height: | 501 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 190.2326° |
| argument of perigee: | 50.4260° |
| revolutions per day: | 15.14942097 |
| mean anomaly at epoch: | 309.9550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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