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 53522U 26145.57171450 +.00000000 +00000-0 +14448-4 0 00003
2 53522 35.0082 194.0081 0006032 47.9423 312.1804 15.23087691 01
| Epoch (UTC): | 25 May 2026 13:43:16 |
| Eccentricity: | 0.0006032 |
| inclination: | 35.0082° |
| perigee height: | 492 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 194.0081° |
| argument of perigee: | 47.9423° |
| revolutions per day: | 15.23087691 |
| mean anomaly at epoch: | 312.1804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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