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 45439U 26145.62558981 +.00000000 +00000-0 -10443-2 0 00005
2 45439 87.8920 25.5498 0001866 81.3945 278.7394 13.11418285 09
| Epoch (UTC): | 25 May 2026 15:00:50 |
| Eccentricity: | 0.0001866 |
| inclination: | 87.8920° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5498° |
| argument of perigee: | 81.3945° |
| revolutions per day: | 13.11418285 |
| mean anomaly at epoch: | 278.7394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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