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 40016U 26088.17718029 +.00000000 +00000-0 +13014-3 0 00005
2 40016 97.7454 237.1361 0044221 335.4524 24.4582 14.79423755 03
| Epoch (UTC): | 29 March 2026 04:15:08 |
| Eccentricity: | 0.0044221 |
| inclination: | 97.7454° |
| perigee height: | 600 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 237.1361° |
| argument of perigee: | 335.4524° |
| revolutions per day: | 14.79423755 |
| mean anomaly at epoch: | 24.4582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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