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 40716U 26145.59833286 +.00000000 +00000-0 +10634-3 0 00000
2 40716 97.6548 13.2140 0007222 123.9579 236.2324 14.85714687 02
| Epoch (UTC): | 25 May 2026 14:21:35 |
| Eccentricity: | 0.0007222 |
| inclination: | 97.6548° |
| perigee height: | 606 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 13.2140° |
| argument of perigee: | 123.9579° |
| revolutions per day: | 14.85714687 |
| mean anomaly at epoch: | 236.2324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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