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 43581U 26145.01805365 +.00000000 +00000-0 +00000-0 0 00000
2 43581 54.0837 183.0913 0005266 288.8293 71.1823 1.86228616 06
| Epoch (UTC): | 25 May 2026 00:25:59 |
| Eccentricity: | 0.0005266 |
| inclination: | 54.0837° |
| perigee height: | 21514 km |
| apogee height: | 21543 km |
| right ascension of ascending node: | 183.0913° |
| argument of perigee: | 288.8293° |
| revolutions per day: | 1.86228616 |
| mean anomaly at epoch: | 71.1823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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