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 26073.92384196 +.00000000 +00000-0 +38368-3 0 00003
2 40014 98.0422 161.0456 0029501 141.0616 219.2747 15.14573493 09
| Epoch (UTC): | 14 March 2026 22:10:19 |
| Eccentricity: | 0.0029501 |
| inclination: | 98.0422° |
| perigee height: | 502 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 161.0456° |
| argument of perigee: | 141.0616° |
| revolutions per day: | 15.14573493 |
| mean anomaly at epoch: | 219.2747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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