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 44067U 26145.60953280 +.00000000 +00000-0 +00000-0 0 00005
2 44067 0.1084 79.8239 0012723 325.0682 188.1286 1.00268627 01
| Epoch (UTC): | 25 May 2026 14:37:43 |
| Eccentricity: | 0.0012723 |
| inclination: | 0.1084° |
| perigee height: | 35734 km |
| apogee height: | 35841 km |
| right ascension of ascending node: | 79.8239° |
| argument of perigee: | 325.0682° |
| revolutions per day: | 1.00268627 |
| mean anomaly at epoch: | 188.1286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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