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 68609U 26145.50003470 +.00000000 +00000-0 +21047-2 0 00005
2 68609 97.2851 345.0014 0001855 94.2925 285.3113 15.49105408 00
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001855 |
| inclination: | 97.2851° |
| perigee height: | 418 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 345.0014° |
| argument of perigee: | 94.2925° |
| revolutions per day: | 15.49105408 |
| mean anomaly at epoch: | 285.3113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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