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 51139U 26145.48236600 +.00000000 +00000-0 -19902-3 0 00004
2 51139 53.2135 314.3937 0001334 86.4577 273.6568 15.08846418 00
| Epoch (UTC): | 25 May 2026 11:34:36 |
| Eccentricity: | 0.0001334 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 314.3937° |
| argument of perigee: | 86.4577° |
| revolutions per day: | 15.08846418 |
| mean anomaly at epoch: | 273.6568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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