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 25159U 26145.40171035 +.00000000 +00000-0 +33078-3 0 00008
2 25159 107.9624 122.5261 0040557 4.1934 355.9539 14.35689433 09
| Epoch (UTC): | 25 May 2026 09:38:27 |
| Eccentricity: | 0.0040557 |
| inclination: | 107.9624° |
| perigee height: | 744 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 122.5261° |
| argument of perigee: | 4.1934° |
| revolutions per day: | 14.35689433 |
| mean anomaly at epoch: | 355.9539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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