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 65164U 26145.60184833 +.00000000 +00000-0 +13819-4 0 00002
2 65164 86.4959 259.6312 0001920 95.6228 264.5125 13.24404292 03
| Epoch (UTC): | 25 May 2026 14:26:39 |
| Eccentricity: | 0.0001920 |
| inclination: | 86.4959° |
| perigee height: | 1166 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 259.6312° |
| argument of perigee: | 95.6228° |
| revolutions per day: | 13.24404292 |
| mean anomaly at epoch: | 264.5125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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