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 40374U 26146.08169703 +.00000000 +00000-0 +00000-0 0 00004
2 40374 4.4790 43.4222 0051238 179.1861 35.0058 1.00272846 04
| Epoch (UTC): | 26 May 2026 01:57:38 |
| Eccentricity: | 0.0051238 |
| inclination: | 4.4790° |
| perigee height: | 35570 km |
| apogee height: | 36002 km |
| right ascension of ascending node: | 43.4222° |
| argument of perigee: | 179.1861° |
| revolutions per day: | 1.00272846 |
| mean anomaly at epoch: | 35.0058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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