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 45156U 26145.41297941 +.00000000 +00000-0 -44438-3 0 00006
2 45156 87.8852 40.7959 0002137 89.5920 270.5452 13.10371014 07
| Epoch (UTC): | 25 May 2026 09:54:41 |
| Eccentricity: | 0.0002137 |
| inclination: | 87.8852° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7959° |
| argument of perigee: | 89.5920° |
| revolutions per day: | 13.10371014 |
| mean anomaly at epoch: | 270.5452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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