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 40938U 26144.79677884 +.00000000 +00000-0 +00000-0 0 00000
2 40938 49.2576 259.0593 0064721 191.3362 175.0261 1.00265134 01
| Epoch (UTC): | 24 May 2026 19:07:21 |
| Eccentricity: | 0.0064721 |
| inclination: | 49.2576° |
| perigee height: | 35516 km |
| apogee height: | 36061 km |
| right ascension of ascending node: | 259.0593° |
| argument of perigee: | 191.3362° |
| revolutions per day: | 1.00265134 |
| mean anomaly at epoch: | 175.0261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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