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 40019U 26106.35689229 +.00000000 +00000-0 +65559-4 0 00000
2 40019 97.9549 234.7317 0080181 110.9524 250.0287 14.70823136 05
| Epoch (UTC): | 16 April 2026 08:33:55 |
| Eccentricity: | 0.0080181 |
| inclination: | 97.9549° |
| perigee height: | 602 km |
| apogee height: | 715 km |
| right ascension of ascending node: | 234.7317° |
| argument of perigee: | 110.9524° |
| revolutions per day: | 14.70823136 |
| mean anomaly at epoch: | 250.0287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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