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 52113U 26145.24772638 +.00000000 +00000-0 -55647-5 0 00005
2 52113 53.2137 95.4388 0001093 93.7067 266.4050 15.08845056 02
| Epoch (UTC): | 25 May 2026 05:56:43 |
| Eccentricity: | 0.0001093 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 95.4388° |
| argument of perigee: | 93.7067° |
| revolutions per day: | 15.08845056 |
| mean anomaly at epoch: | 266.4050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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