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 26110.58456058 +.00000000 +00000-0 +13448-3 0 00009
2 40017 98.0266 181.3208 0012683 57.2431 303.0021 15.16848510 08
| Epoch (UTC): | 20 April 2026 14:01:46 |
| Eccentricity: | 0.0012683 |
| inclination: | 98.0266° |
| perigee height: | 507 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 181.3208° |
| argument of perigee: | 57.2431° |
| revolutions per day: | 15.16848510 |
| mean anomaly at epoch: | 303.0021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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