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 26066.98661957 +.00000000 +00000-0 +48896-3 0 00001
2 40014 98.0429 153.7137 0029207 164.2632 195.9513 15.14470230 04
| Epoch (UTC): | 07 March 2026 23:40:43 |
| Eccentricity: | 0.0029207 |
| inclination: | 98.0429° |
| perigee height: | 502 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 153.7137° |
| argument of perigee: | 164.2632° |
| revolutions per day: | 15.14470230 |
| mean anomaly at epoch: | 195.9513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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