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 62515U 26145.51813656 +.00000000 +00000-0 +19913-2 0 00000
2 62515 42.9988 327.4535 0002239 238.9845 121.0803 15.70905654 02
| Epoch (UTC): | 25 May 2026 12:26:06 |
| Eccentricity: | 0.0002239 |
| inclination: | 42.9988° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 327.4535° |
| argument of perigee: | 238.9845° |
| revolutions per day: | 15.70905654 |
| mean anomaly at epoch: | 121.0803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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