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 62135U 26145.18713453 +.00000000 +00000-0 +72414-3 0 00001
2 62135 43.0013 64.5598 0001366 268.0272 92.0424 15.27620727 00
| Epoch (UTC): | 25 May 2026 04:29:28 |
| Eccentricity: | 0.0001366 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 64.5598° |
| argument of perigee: | 268.0272° |
| revolutions per day: | 15.27620727 |
| mean anomaly at epoch: | 92.0424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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