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 45143U 26145.24206635 +.00000000 +00000-0 -47146-1 0 00000
2 45143 87.8848 40.8378 0001801 72.5340 287.5984 13.10470784 01
| Epoch (UTC): | 25 May 2026 05:48:34 |
| Eccentricity: | 0.0001801 |
| inclination: | 87.8848° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8378° |
| argument of perigee: | 72.5340° |
| revolutions per day: | 13.10470784 |
| mean anomaly at epoch: | 287.5984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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