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 45190U 26144.88849170 +.00000000 +00000-0 +47319-3 0 00001
2 45190 53.0410 309.6712 0006102 183.6141 176.4833 15.72229266 09
| Epoch (UTC): | 24 May 2026 21:19:25 |
| Eccentricity: | 0.0006102 |
| inclination: | 53.0410° |
| perigee height: | 348 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 309.6712° |
| argument of perigee: | 183.6141° |
| revolutions per day: | 15.72229266 |
| mean anomaly at epoch: | 176.4833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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