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 45435U 26145.62401927 +.00000000 +00000-0 -11508-2 0 00001
2 45435 87.8917 25.5477 0001731 79.9175 280.2148 13.11417089 03
| Epoch (UTC): | 25 May 2026 14:58:35 |
| Eccentricity: | 0.0001731 |
| inclination: | 87.8917° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5477° |
| argument of perigee: | 79.9175° |
| revolutions per day: | 13.11417089 |
| mean anomaly at epoch: | 280.2148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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