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 62872U 26145.34303936 +.00000000 +00000-0 +88982-3 0 00005
2 62872 53.1591 133.7469 0001075 91.1410 268.9715 15.33555753 03
| Epoch (UTC): | 25 May 2026 08:13:58 |
| Eccentricity: | 0.0001075 |
| inclination: | 53.1591° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 133.7469° |
| argument of perigee: | 91.1410° |
| revolutions per day: | 15.33555753 |
| mean anomaly at epoch: | 268.9715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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