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 61605U 26145.46098909 +.00000000 +00000-0 +16347-2 0 00007
2 61605 87.8856 40.7904 0001143 78.1931 281.9325 13.10374439 09
| Epoch (UTC): | 25 May 2026 11:03:49 |
| Eccentricity: | 0.0001143 |
| inclination: | 87.8856° |
| perigee height: | 1221 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7904° |
| argument of perigee: | 78.1931° |
| revolutions per day: | 13.10374439 |
| mean anomaly at epoch: | 281.9325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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