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 45669U 26145.05435095 +.00000000 +00000-0 +10970-2 0 00001
2 45669 53.0269 14.7396 0000847 227.6379 132.4559 15.56039096 05
| Epoch (UTC): | 25 May 2026 01:18:15 |
| Eccentricity: | 0.0000847 |
| inclination: | 53.0269° |
| perigee height: | 399 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 14.7396° |
| argument of perigee: | 227.6379° |
| revolutions per day: | 15.56039096 |
| mean anomaly at epoch: | 132.4559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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