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 41589U 26144.91875073 +.00000000 +00000-0 +00000-0 0 00007
2 41589 0.0091 148.4920 0000051 259.1369 48.6439 1.00270666 00
| Epoch (UTC): | 24 May 2026 22:03:00 |
| Eccentricity: | 0.0000051 |
| inclination: | 0.0091° |
| perigee height: | 35787 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 148.4920° |
| argument of perigee: | 259.1369° |
| revolutions per day: | 1.00270666 |
| mean anomaly at epoch: | 48.6439° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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