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 61224U 26145.51988426 +.00000000 +00000-0 +27503-3 0 00009
2 61224 98.0409 235.7793 0003135 124.5677 235.5827 14.72323511 08
| Epoch (UTC): | 25 May 2026 12:28:38 |
| Eccentricity: | 0.0003135 |
| inclination: | 98.0409° |
| perigee height: | 651 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 235.7793° |
| argument of perigee: | 124.5677° |
| revolutions per day: | 14.72323511 |
| mean anomaly at epoch: | 235.5827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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