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 26138.52074103 +.00000000 +00000-0 +21579-3 0 00001
2 40014 98.0422 229.3439 0026771 282.4910 77.3325 15.15249437 05
| Epoch (UTC): | 18 May 2026 12:29:52 |
| Eccentricity: | 0.0026771 |
| inclination: | 98.0422° |
| perigee height: | 502 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 229.3439° |
| argument of perigee: | 282.4910° |
| revolutions per day: | 15.15249437 |
| mean anomaly at epoch: | 77.3325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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