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 45159U 26145.45254561 +.00000000 +00000-0 +73704-3 0 00001
2 45159 87.8864 40.7853 0001731 88.3107 271.8219 13.10370646 04
| Epoch (UTC): | 25 May 2026 10:51:39 |
| Eccentricity: | 0.0001731 |
| inclination: | 87.8864° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7853° |
| argument of perigee: | 88.3107° |
| revolutions per day: | 13.10370646 |
| mean anomaly at epoch: | 271.8219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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