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 25134U 26033.42475544 +.00000000 +00000-0 +00000-0 0 00007
2 25134 12.7185 11.6126 0003915 216.9469 143.2442 0.99149765 03
| Epoch (UTC): | 02 February 2026 10:11:38 |
| Eccentricity: | 0.0003915 |
| inclination: | 12.7185° |
| perigee height: | 36087 km |
| apogee height: | 36121 km |
| right ascension of ascending node: | 11.6126° |
| argument of perigee: | 216.9469° |
| revolutions per day: | 0.99149765 |
| mean anomaly at epoch: | 143.2442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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