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 41174U 26143.98872667 +.00000000 +00000-0 +00000-0 0 00009
2 41174 55.8138 101.9249 0005590 335.9950 23.9396 1.70473875 02
| Epoch (UTC): | 23 May 2026 23:43:45 |
| Eccentricity: | 0.0005590 |
| inclination: | 55.8138° |
| perigee height: | 23206 km |
| apogee height: | 23239 km |
| right ascension of ascending node: | 101.9249° |
| argument of perigee: | 335.9950° |
| revolutions per day: | 1.70473875 |
| mean anomaly at epoch: | 23.9396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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