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 26160.30659075 +.00000000 +00000-0 +15564-3 0 00005
2 41634 75.0025 293.8918 0007068 49.0017 311.1782 14.93552618 08
| Epoch (UTC): | 09 June 2026 07:21:29 |
| Eccentricity: | 0.0007068 |
| inclination: | 75.0025° |
| perigee height: | 582 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 293.8918° |
| argument of perigee: | 49.0017° |
| revolutions per day: | 14.93552618 |
| mean anomaly at epoch: | 311.1782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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