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 45433U 26145.60185164 +.00000000 +00000-0 -74790-3 0 00002
2 45433 87.8907 25.5604 0001618 83.7079 276.4233 13.11415430 02
| Epoch (UTC): | 25 May 2026 14:26:39 |
| Eccentricity: | 0.0001618 |
| inclination: | 87.8907° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5604° |
| argument of perigee: | 83.7079° |
| revolutions per day: | 13.11415430 |
| mean anomaly at epoch: | 276.4233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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