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 26073.59350736 +.00000000 +00000-0 +42069-3 0 00002
2 40014 98.0424 160.6968 0029521 142.1948 218.1364 15.14570229 03
| Epoch (UTC): | 14 March 2026 14:14:39 |
| Eccentricity: | 0.0029521 |
| inclination: | 98.0424° |
| perigee height: | 502 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 160.6968° |
| argument of perigee: | 142.1948° |
| revolutions per day: | 15.14570229 |
| mean anomaly at epoch: | 218.1364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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