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 40017U 26156.68700603 +.00000000 +00000-0 +30923-3 0 00005
2 40017 98.0238 230.1341 0010256 251.8759 108.1357 15.17444616 03
| Epoch (UTC): | 05 June 2026 16:29:17 |
| Eccentricity: | 0.0010256 |
| inclination: | 98.0238° |
| perigee height: | 506 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 230.1341° |
| argument of perigee: | 251.8759° |
| revolutions per day: | 15.17444616 |
| mean anomaly at epoch: | 108.1357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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