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 26135.16618095 +.00000000 +00000-0 +87007-4 0 00002
2 25544 51.6313 103.5621 0007452 60.7339 299.4393 15.49219006 01
| Epoch (UTC): | 15 May 2026 03:59:18 |
| Eccentricity: | 0.0007452 |
| inclination: | 51.6313° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 103.5621° |
| argument of perigee: | 60.7339° |
| revolutions per day: | 15.49219006 |
| mean anomaly at epoch: | 299.4393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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