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 45139U 26145.42213139 +.00000000 +00000-0 +14062-2 0 00003
2 45139 87.8915 25.5980 0001651 83.1396 276.9920 13.11415953 02
| Epoch (UTC): | 25 May 2026 10:07:52 |
| Eccentricity: | 0.0001651 |
| inclination: | 87.8915° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5980° |
| argument of perigee: | 83.1396° |
| revolutions per day: | 13.11415953 |
| mean anomaly at epoch: | 276.9920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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