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 41175U 26126.61144964 +.00000000 +00000-0 +00000-0 0 00003
2 41175 55.8012 102.3981 0005042 331.9536 27.9874 1.70474018 05
| Epoch (UTC): | 06 May 2026 14:40:29 |
| Eccentricity: | 0.0005042 |
| inclination: | 55.8012° |
| perigee height: | 23207 km |
| apogee height: | 23237 km |
| right ascension of ascending node: | 102.3981° |
| argument of perigee: | 331.9536° |
| revolutions per day: | 1.70474018 |
| mean anomaly at epoch: | 27.9874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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