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 45450U 26145.34614601 +.00000000 +00000-0 +96073-4 0 00003
2 45450 87.9161 10.3894 0001784 77.2504 282.8827 13.17650102 05
| Epoch (UTC): | 25 May 2026 08:18:27 |
| Eccentricity: | 0.0001784 |
| inclination: | 87.9161° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3894° |
| argument of perigee: | 77.2504° |
| revolutions per day: | 13.17650102 |
| mean anomaly at epoch: | 282.8827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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