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 51135U 26145.48971288 +.00000000 +00000-0 +64222-4 0 00003
2 51135 53.2137 314.2463 0001558 88.5927 271.5244 15.08837744 01
| Epoch (UTC): | 25 May 2026 11:45:11 |
| Eccentricity: | 0.0001558 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 314.2463° |
| argument of perigee: | 88.5927° |
| revolutions per day: | 15.08837744 |
| mean anomaly at epoch: | 271.5244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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