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 41592U 26144.97405737 +.00000000 +00000-0 +00000-0 0 00003
2 41592 0.0150 322.3747 0001572 105.5065 103.9719 1.00269056 03
| Epoch (UTC): | 24 May 2026 23:22:38 |
| Eccentricity: | 0.0001572 |
| inclination: | 0.0150° |
| perigee height: | 35781 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 322.3747° |
| argument of perigee: | 105.5065° |
| revolutions per day: | 1.00269056 |
| mean anomaly at epoch: | 103.9719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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