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 25544U 26151.16242250 +.00000000 +00000-0 +23226-3 0 00008
2 25544 51.6337 24.3812 0007232 116.8819 243.2910 15.49515140 01
| Epoch (UTC): | 31 May 2026 03:53:53 |
| Eccentricity: | 0.0007232 |
| inclination: | 51.6337° |
| perigee height: | 413 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 24.3812° |
| argument of perigee: | 116.8819° |
| revolutions per day: | 15.49515140 |
| mean anomaly at epoch: | 243.2910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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