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 40013U 26118.47541262 +.00000000 +00000-0 +22113-3 0 00002
2 40013 97.5902 354.6972 0002352 98.8519 261.2968 14.93585607 02
| Epoch (UTC): | 28 April 2026 11:24:35 |
| Eccentricity: | 0.0002352 |
| inclination: | 97.5902° |
| perigee height: | 585 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 354.6972° |
| argument of perigee: | 98.8519° |
| revolutions per day: | 14.93585607 |
| mean anomaly at epoch: | 261.2968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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