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 26065.86340141 +.00000000 +00000-0 +32122-3 0 00001
2 40014 98.0430 152.5272 0029053 167.9197 192.2736 15.14447796 06
| Epoch (UTC): | 06 March 2026 20:43:17 |
| Eccentricity: | 0.0029053 |
| inclination: | 98.0430° |
| perigee height: | 503 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 152.5272° |
| argument of perigee: | 167.9197° |
| revolutions per day: | 15.14447796 |
| mean anomaly at epoch: | 192.2736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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