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 51136U 26145.48139433 +.00000000 +00000-0 -20352-4 0 00009
2 51136 53.2145 314.1848 0001071 98.1928 261.9186 15.08837347 02
| Epoch (UTC): | 25 May 2026 11:33:12 |
| Eccentricity: | 0.0001071 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 314.1848° |
| argument of perigee: | 98.1928° |
| revolutions per day: | 15.08837347 |
| mean anomaly at epoch: | 261.9186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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