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 40071U 26150.49776405 +.00000000 +00000-0 +14084-3 0 00001
2 40071 98.3850 111.1280 0006603 341.4220 18.6754 14.89920424 06
| Epoch (UTC): | 30 May 2026 11:56:46 |
| Eccentricity: | 0.0006603 |
| inclination: | 98.3850° |
| perigee height: | 594 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 111.1280° |
| argument of perigee: | 341.4220° |
| revolutions per day: | 14.89920424 |
| mean anomaly at epoch: | 18.6754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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