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 40425U 26144.70547051 +.00000000 +00000-0 +00000-0 0 00004
2 40425 0.0099 140.0314 0000142 305.5978 295.7518 1.00269784 06
| Epoch (UTC): | 24 May 2026 16:55:52 |
| Eccentricity: | 0.0000142 |
| inclination: | 0.0099° |
| perigee height: | 35787 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 140.0314° |
| argument of perigee: | 305.5978° |
| revolutions per day: | 1.00269784 |
| mean anomaly at epoch: | 295.7518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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