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 26145.59517660 +.00000000 +00000-0 +15980-3 0 00008
2 40071 98.3855 105.9297 0007174 359.1005 1.0197 14.89903817 05
| Epoch (UTC): | 25 May 2026 14:17:03 |
| Eccentricity: | 0.0007174 |
| inclination: | 98.3855° |
| perigee height: | 593 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 105.9297° |
| argument of perigee: | 359.1005° |
| revolutions per day: | 14.89903817 |
| mean anomaly at epoch: | 1.0197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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