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 61012U 26145.57735939 +.00000000 +00000-0 +18219-3 0 00003
2 61012 49.9930 188.1937 0019371 328.3928 31.5846 14.84151747 08
| Epoch (UTC): | 25 May 2026 13:51:23 |
| Eccentricity: | 0.0019371 |
| inclination: | 49.9930° |
| perigee height: | 603 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 188.1937° |
| argument of perigee: | 328.3928° |
| revolutions per day: | 14.84151747 |
| mean anomaly at epoch: | 31.5846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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