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 61596U 26145.32674214 +.00000000 +00000-0 +21498-3 0 00004
2 61596 87.9148 10.4238 0003064 86.5363 273.6119 13.17651894 02
| Epoch (UTC): | 25 May 2026 07:50:30 |
| Eccentricity: | 0.0003064 |
| inclination: | 87.9148° |
| perigee height: | 1191 km |
| apogee height: | 1196 km |
| right ascension of ascending node: | 10.4238° |
| argument of perigee: | 86.5363° |
| revolutions per day: | 13.17651894 |
| mean anomaly at epoch: | 273.6119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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