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 66721U 26145.57734926 +.00000000 +00000-0 +27635-3 0 00002
2 66721 97.4183 219.3888 0005573 104.7869 255.3984 15.19461615 05
| Epoch (UTC): | 25 May 2026 13:51:22 |
| Eccentricity: | 0.0005573 |
| inclination: | 97.4183° |
| perigee height: | 504 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 219.3888° |
| argument of perigee: | 104.7869° |
| revolutions per day: | 15.19461615 |
| mean anomaly at epoch: | 255.3984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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