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 68581U 26145.58335647 +.00000000 +00000-0 -34439-2 0 00006
2 68581 51.8959 289.7342 0005155 337.6501 350.1454 14.90896556 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0005155 |
| inclination: | 51.8959° |
| perigee height: | 592 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 289.7342° |
| argument of perigee: | 337.6501° |
| revolutions per day: | 14.90896556 |
| mean anomaly at epoch: | 350.1454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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