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 45440U 26145.13350372 +.00000000 +00000-0 +19991-3 0 00004
2 45440 87.8926 25.6229 0001828 84.3194 275.8143 13.11909388 06
| Epoch (UTC): | 25 May 2026 03:12:14 |
| Eccentricity: | 0.0001828 |
| inclination: | 87.8926° |
| perigee height: | 1214 km |
| apogee height: | 1217 km |
| right ascension of ascending node: | 25.6229° |
| argument of perigee: | 84.3194° |
| revolutions per day: | 13.11909388 |
| mean anomaly at epoch: | 275.8143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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