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 45448U 26145.13233505 +.00000000 +00000-0 +44272-3 0 00000
2 45448 87.8917 25.6536 0001945 90.6683 269.4667 13.11413886 01
| Epoch (UTC): | 25 May 2026 03:10:33 |
| Eccentricity: | 0.0001945 |
| inclination: | 87.8917° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6536° |
| argument of perigee: | 90.6683° |
| revolutions per day: | 13.11413886 |
| mean anomaly at epoch: | 269.4667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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