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 41727U 26145.60547110 +.00000000 +00000-0 +28906-4 0 00005
2 41727 98.4021 153.7329 0000953 90.4177 269.7122 14.42211888 00
| Epoch (UTC): | 25 May 2026 14:31:52 |
| Eccentricity: | 0.0000953 |
| inclination: | 98.4021° |
| perigee height: | 751 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 153.7329° |
| argument of perigee: | 90.4177° |
| revolutions per day: | 14.42211888 |
| mean anomaly at epoch: | 269.7122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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