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 26064.30665943 +.00000000 +00000-0 +17388-3 0 00005
2 41634 75.0009 115.5738 0008616 284.8692 75.1542 14.93220417 08
| Epoch (UTC): | 05 March 2026 07:21:35 |
| Eccentricity: | 0.0008616 |
| inclination: | 75.0009° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 115.5738° |
| argument of perigee: | 284.8692° |
| revolutions per day: | 14.93220417 |
| mean anomaly at epoch: | 75.1542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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