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 61562U 26145.56173359 +.00000000 +00000-0 +93225-4 0 00005
2 61562 88.9812 64.3654 0008187 305.0326 55.0057 13.51069825 01
| Epoch (UTC): | 25 May 2026 13:28:53 |
| Eccentricity: | 0.0008187 |
| inclination: | 88.9812° |
| perigee height: | 1062 km |
| apogee height: | 1074 km |
| right ascension of ascending node: | 64.3654° |
| argument of perigee: | 305.0326° |
| revolutions per day: | 13.51069825 |
| mean anomaly at epoch: | 55.0057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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