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 26154.18097634 +.00000000 +00000-0 +00000-0 0 00007
2 41175 55.8180 101.6428 0004857 341.4145 18.5225 1.70473818 07
| Epoch (UTC): | 03 June 2026 04:20:36 |
| Eccentricity: | 0.0004857 |
| inclination: | 55.8180° |
| perigee height: | 23208 km |
| apogee height: | 23237 km |
| right ascension of ascending node: | 101.6428° |
| argument of perigee: | 341.4145° |
| revolutions per day: | 1.70473818 |
| mean anomaly at epoch: | 18.5225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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