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 59651U 26145.47253472 +.00000000 +00000-0 +65200-5 0 00009
2 59651 42.9995 66.2839 0000922 258.8368 101.2380 15.27578192 05
| Epoch (UTC): | 25 May 2026 11:20:27 |
| Eccentricity: | 0.0000922 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.2839° |
| argument of perigee: | 258.8368° |
| revolutions per day: | 15.27578192 |
| mean anomaly at epoch: | 101.2380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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