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 40056U 26145.58836703 +.00000000 +00000-0 +10831-3 0 00002
2 40056 98.3154 20.1113 0014149 84.5523 275.7302 14.81232207 07
| Epoch (UTC): | 25 May 2026 14:07:14 |
| Eccentricity: | 0.0014149 |
| inclination: | 98.3154° |
| perigee height: | 616 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 20.1113° |
| argument of perigee: | 84.5523° |
| revolutions per day: | 14.81232207 |
| mean anomaly at epoch: | 275.7302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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