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 61222U 26145.48550539 +.00000000 +00000-0 +27638-3 0 00002
2 61222 98.0417 235.6204 0001398 124.4017 235.7323 14.72288126 02
| Epoch (UTC): | 25 May 2026 11:39:07 |
| Eccentricity: | 0.0001398 |
| inclination: | 98.0417° |
| perigee height: | 653 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 235.6204° |
| argument of perigee: | 124.4017° |
| revolutions per day: | 14.72288126 |
| mean anomaly at epoch: | 235.7323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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