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 45589U 26145.58335647 +.00000000 +00000-0 +45744-2 0 00009
2 45589 53.0430 50.7389 0001753 76.1455 51.6837 15.67120259 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001753 |
| inclination: | 53.0430° |
| perigee height: | 366 km |
| apogee height: | 368 km |
| right ascension of ascending node: | 50.7389° |
| argument of perigee: | 76.1455° |
| revolutions per day: | 15.67120259 |
| mean anomaly at epoch: | 51.6837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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