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 26101.26826549 +.00000000 +00000-0 +13873-3 0 00002
2 40071 98.3810 58.9466 0008166 123.2676 236.9323 14.89776472 02
| Epoch (UTC): | 11 April 2026 06:26:18 |
| Eccentricity: | 0.0008166 |
| inclination: | 98.3810° |
| perigee height: | 593 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 58.9466° |
| argument of perigee: | 123.2676° |
| revolutions per day: | 14.89776472 |
| mean anomaly at epoch: | 236.9323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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