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 59650U 26145.46482731 +.00000000 +00000-0 +19244-4 0 00005
2 59650 43.0010 66.2252 0000765 263.3620 96.7145 15.27575411 08
| Epoch (UTC): | 25 May 2026 11:09:21 |
| Eccentricity: | 0.0000765 |
| inclination: | 43.0010° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.2252° |
| argument of perigee: | 263.3620° |
| revolutions per day: | 15.27575411 |
| mean anomaly at epoch: | 96.7145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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