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 41588U 26144.95688330 +.00000000 +00000-0 +00000-0 0 00008
2 41588 0.0160 290.5246 0001601 75.6348 295.5967 1.00267480 05
| Epoch (UTC): | 24 May 2026 22:57:54 |
| Eccentricity: | 0.0001601 |
| inclination: | 0.0160° |
| perigee height: | 35781 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 290.5246° |
| argument of perigee: | 75.6348° |
| revolutions per day: | 1.00267480 |
| mean anomaly at epoch: | 295.5967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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