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 26145.58060843 +.00000000 +00000-0 +00000-0 0 00003
2 40374 4.4781 43.4198 0051215 179.2088 214.0981 1.00272872 06
| Epoch (UTC): | 25 May 2026 13:56:04 |
| Eccentricity: | 0.0051215 |
| inclination: | 4.4781° |
| perigee height: | 35570 km |
| apogee height: | 36002 km |
| right ascension of ascending node: | 43.4198° |
| argument of perigee: | 179.2088° |
| revolutions per day: | 1.00272872 |
| mean anomaly at epoch: | 214.0981° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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