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 62961U 26145.24072520 +.00000000 +00000-0 +79062-3 0 00004
2 62961 53.1593 237.1882 0001485 89.4852 270.6319 15.30214851 05
| Epoch (UTC): | 25 May 2026 05:46:38 |
| Eccentricity: | 0.0001485 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 237.1882° |
| argument of perigee: | 89.4852° |
| revolutions per day: | 15.30214851 |
| mean anomaly at epoch: | 270.6319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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