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 52496U 26145.48463141 +.00000000 +00000-0 +14924-3 0 00001
2 52496 53.2124 59.3745 0001146 85.9282 274.1842 15.08829125 03
| Epoch (UTC): | 25 May 2026 11:37:52 |
| Eccentricity: | 0.0001146 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 59.3745° |
| argument of perigee: | 85.9282° |
| revolutions per day: | 15.08829125 |
| mean anomaly at epoch: | 274.1842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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