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 26110.60412516 +.00000000 +00000-0 +67058-4 0 00000
2 40071 98.3831 68.8381 0008525 96.8738 263.3448 14.89794770 07
| Epoch (UTC): | 20 April 2026 14:29:56 |
| Eccentricity: | 0.0008525 |
| inclination: | 98.3831° |
| perigee height: | 593 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 68.8381° |
| argument of perigee: | 96.8738° |
| revolutions per day: | 14.89794770 |
| mean anomaly at epoch: | 263.3448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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