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 62652U 26145.17838995 +.00000000 +00000-0 +37504-3 0 00004
2 62652 97.3966 226.8917 0002721 75.9699 284.1844 15.28558387 08
| Epoch (UTC): | 25 May 2026 04:16:52 |
| Eccentricity: | 0.0002721 |
| inclination: | 97.3966° |
| perigee height: | 478 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 226.8917° |
| argument of perigee: | 75.9699° |
| revolutions per day: | 15.28558387 |
| mean anomaly at epoch: | 284.1844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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