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 26106.95630249 +.00000000 +00000-0 +13333-3 0 00004
2 40017 98.0274 177.4807 0012867 68.7415 291.5190 15.16808018 08
| Epoch (UTC): | 16 April 2026 22:57:04 |
| Eccentricity: | 0.0012867 |
| inclination: | 98.0274° |
| perigee height: | 507 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 177.4807° |
| argument of perigee: | 68.7415° |
| revolutions per day: | 15.16808018 |
| mean anomaly at epoch: | 291.5190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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