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 25157U 26053.84055976 +.00000000 +00000-0 +84551-3 0 00009
2 25157 108.0177 229.9550 0054261 224.0480 135.6397 15.63404960 08
| Epoch (UTC): | 22 February 2026 20:10:24 |
| Eccentricity: | 0.0054261 |
| inclination: | 108.0177° |
| perigee height: | 341 km |
| apogee height: | 414 km |
| right ascension of ascending node: | 229.9550° |
| argument of perigee: | 224.0480° |
| revolutions per day: | 15.63404960 |
| mean anomaly at epoch: | 135.6397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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