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 61736U 26145.51283147 +.00000000 +00000-0 +37017-4 0 00007
2 61736 98.7202 18.8321 0001794 61.9970 298.1389 14.22752623 03
| Epoch (UTC): | 25 May 2026 12:18:28 |
| Eccentricity: | 0.0001794 |
| inclination: | 98.7202° |
| perigee height: | 815 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 18.8321° |
| argument of perigee: | 61.9970° |
| revolutions per day: | 14.22752623 |
| mean anomaly at epoch: | 298.1389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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