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 12139U 26127.82620949 +.00000000 +00000-0 +23775-3 0 00004
2 12139 82.9400 235.2382 0253366 332.8590 25.9577 15.13197048 05
| Epoch (UTC): | 07 May 2026 19:49:44 |
| Eccentricity: | 0.0253366 |
| inclination: | 82.9400° |
| perigee height: | 352 km |
| apogee height: | 701 km |
| right ascension of ascending node: | 235.2382° |
| argument of perigee: | 332.8590° |
| revolutions per day: | 15.13197048 |
| mean anomaly at epoch: | 25.9577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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