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 26128.21996869 +.00000000 +00000-0 +13392-3 0 00001
2 41634 75.0046 354.6303 0007227 137.8697 222.3049 14.93485671 05
| Epoch (UTC): | 08 May 2026 05:16:45 |
| Eccentricity: | 0.0007227 |
| inclination: | 75.0046° |
| perigee height: | 582 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 354.6303° |
| argument of perigee: | 137.8697° |
| revolutions per day: | 14.93485671 |
| mean anomaly at epoch: | 222.3049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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