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 45444U 26145.41719027 +.00000000 +00000-0 +13312-2 0 00005
2 45444 87.8918 25.5887 0002159 77.9502 282.1868 13.11418612 09
| Epoch (UTC): | 25 May 2026 10:00:45 |
| Eccentricity: | 0.0002159 |
| inclination: | 87.8918° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5887° |
| argument of perigee: | 77.9502° |
| revolutions per day: | 13.11418612 |
| mean anomaly at epoch: | 282.1868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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