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 26108.93387053 +.00000000 +00000-0 +15107-3 0 00004
2 40014 98.0407 198.0541 0028785 25.8239 334.4421 15.14983714 00
| Epoch (UTC): | 18 April 2026 22:24:46 |
| Eccentricity: | 0.0028785 |
| inclination: | 98.0407° |
| perigee height: | 501 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 198.0541° |
| argument of perigee: | 25.8239° |
| revolutions per day: | 15.14983714 |
| mean anomaly at epoch: | 334.4421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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