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 26053.83757821 +.00000000 +00000-0 +34494-3 0 00006
2 40014 98.0449 139.8181 0028381 209.1501 150.8146 15.14279092 01
| Epoch (UTC): | 22 February 2026 20:06:06 |
| Eccentricity: | 0.0028381 |
| inclination: | 98.0449° |
| perigee height: | 504 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 139.8181° |
| argument of perigee: | 209.1501° |
| revolutions per day: | 15.14279092 |
| mean anomaly at epoch: | 150.8146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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