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 26071.67754962 +.00000000 +00000-0 +44265-3 0 00008
2 40014 98.0423 158.6715 0029443 148.2641 212.0372 15.14547253 02
| Epoch (UTC): | 12 March 2026 16:15:40 |
| Eccentricity: | 0.0029443 |
| inclination: | 98.0423° |
| perigee height: | 502 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 158.6715° |
| argument of perigee: | 148.2641° |
| revolutions per day: | 15.14547253 |
| mean anomaly at epoch: | 212.0372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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