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 45389U 26145.55416516 +.00000000 +00000-0 +48866-3 0 00008
2 45389 53.0393 92.8192 0004373 75.6156 284.5346 15.69187858 02
| Epoch (UTC): | 25 May 2026 13:17:59 |
| Eccentricity: | 0.0004373 |
| inclination: | 53.0393° |
| perigee height: | 358 km |
| apogee height: | 364 km |
| right ascension of ascending node: | 92.8192° |
| argument of perigee: | 75.6156° |
| revolutions per day: | 15.69187858 |
| mean anomaly at epoch: | 284.5346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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