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 40146U 26145.61711272 +.00000000 +00000-0 +00000-0 0 00003
2 40146 0.0337 85.4134 0002059 337.0791 198.8812 1.00271008 07
| Epoch (UTC): | 25 May 2026 14:48:38 |
| Eccentricity: | 0.0002059 |
| inclination: | 0.0337° |
| perigee height: | 35778 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 85.4134° |
| argument of perigee: | 337.0791° |
| revolutions per day: | 1.00271008 |
| mean anomaly at epoch: | 198.8812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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