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 40013U 26145.60758647 +.00000000 +00000-0 +16560-3 0 00003
2 40013 97.5859 20.8867 0002408 72.6077 287.5406 14.93652386 06
| Epoch (UTC): | 25 May 2026 14:34:55 |
| Eccentricity: | 0.0002408 |
| inclination: | 97.5859° |
| perigee height: | 585 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 20.8867° |
| argument of perigee: | 72.6077° |
| revolutions per day: | 14.93652386 |
| mean anomaly at epoch: | 287.5406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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