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 26075.83050008 +.00000000 +00000-0 +95290-4 0 00004
2 41634 75.0012 93.7683 0008657 260.3701 99.6510 14.93247172 06
| Epoch (UTC): | 16 March 2026 19:55:55 |
| Eccentricity: | 0.0008657 |
| inclination: | 75.0012° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 93.7683° |
| argument of perigee: | 260.3701° |
| revolutions per day: | 14.93247172 |
| mean anomaly at epoch: | 99.6510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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