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 26138.19793205 +.00000000 +00000-0 +12105-3 0 00001
2 25544 51.6325 88.5573 0007513 70.6653 289.5148 15.49256023 07
| Epoch (UTC): | 18 May 2026 04:45:01 |
| Eccentricity: | 0.0007513 |
| inclination: | 51.6325° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 88.5573° |
| argument of perigee: | 70.6653° |
| revolutions per day: | 15.49256023 |
| mean anomaly at epoch: | 289.5148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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