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 45027U 26145.22873890 +.00000000 +00000-0 +00000-0 0 00008
2 45027 0.0713 98.1925 0000904 171.0915 63.0846 1.00270551 00
| Epoch (UTC): | 25 May 2026 05:29:23 |
| Eccentricity: | 0.0000904 |
| inclination: | 0.0713° |
| perigee height: | 35783 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 98.1925° |
| argument of perigee: | 171.0915° |
| revolutions per day: | 1.00270551 |
| mean anomaly at epoch: | 63.0846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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