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 65159U 26145.40355719 +.00000000 +00000-0 +35086-4 0 00007
2 65159 98.6655 205.5457 0001084 83.2284 276.9017 14.21505390 07
| Epoch (UTC): | 25 May 2026 09:41:07 |
| Eccentricity: | 0.0001084 |
| inclination: | 98.6655° |
| perigee height: | 819 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 205.5457° |
| argument of perigee: | 83.2284° |
| revolutions per day: | 14.21505390 |
| mean anomaly at epoch: | 276.9017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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