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 53264U 26145.44506403 +.00000000 +00000-0 +66387-4 0 00001
2 53264 53.2130 209.5516 0001030 77.8243 282.2864 15.08841014 03
| Epoch (UTC): | 25 May 2026 10:40:53 |
| Eccentricity: | 0.0001030 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 209.5516° |
| argument of perigee: | 77.8243° |
| revolutions per day: | 15.08841014 |
| mean anomaly at epoch: | 282.2864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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