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 53135U 26145.38802604 +.00000000 +00000-0 +28877-4 0 00005
2 53135 53.2140 189.8078 0001107 87.9628 272.1491 15.08840289 05
| Epoch (UTC): | 25 May 2026 09:18:45 |
| Eccentricity: | 0.0001107 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 189.8078° |
| argument of perigee: | 87.9628° |
| revolutions per day: | 15.08840289 |
| mean anomaly at epoch: | 272.1491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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