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 59687U 26145.57991441 +.00000000 +00000-0 +17976-3 0 00009
2 59687 42.9991 345.4844 0000850 293.9515 66.1247 15.27584462 00
| Epoch (UTC): | 25 May 2026 13:55:04 |
| Eccentricity: | 0.0000850 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.4844° |
| argument of perigee: | 293.9515° |
| revolutions per day: | 15.27584462 |
| mean anomaly at epoch: | 66.1247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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