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 68590U 26145.11390089 +.00000000 +00000-0 +79650-3 0 00000
2 68590 51.8746 288.2868 0004485 282.8180 77.2306 15.38634482 02
| Epoch (UTC): | 25 May 2026 02:44:01 |
| Eccentricity: | 0.0004485 |
| inclination: | 51.8746° |
| perigee height: | 447 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 288.2868° |
| argument of perigee: | 282.8180° |
| revolutions per day: | 15.38634482 |
| mean anomaly at epoch: | 77.2306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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