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 25160U 26129.28338116 +.00000000 +00000-0 +73236-4 0 00004
2 25160 108.0081 253.7725 0062733 201.0022 179.4112 14.22473294 06
| Epoch (UTC): | 09 May 2026 06:48:04 |
| Eccentricity: | 0.0062733 |
| inclination: | 108.0081° |
| perigee height: | 772 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 253.7725° |
| argument of perigee: | 201.0022° |
| revolutions per day: | 14.22473294 |
| mean anomaly at epoch: | 179.4112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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