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 41634U 26064.77565720 +.00000000 +00000-0 +15980-3 0 00004
2 41634 75.0009 114.6864 0008623 283.9028 76.1201 14.93221607 04
| Epoch (UTC): | 05 March 2026 18:36:56 |
| Eccentricity: | 0.0008623 |
| inclination: | 75.0009° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 114.6864° |
| argument of perigee: | 283.9028° |
| revolutions per day: | 14.93221607 |
| mean anomaly at epoch: | 76.1201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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