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 66825U 26145.33818551 +.00000000 +00000-0 +14884-3 0 00000
2 66825 70.0004 141.3395 0003805 266.5554 93.5170 14.98334043 09
| Epoch (UTC): | 25 May 2026 08:06:59 |
| Eccentricity: | 0.0003805 |
| inclination: | 70.0004° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.3395° |
| argument of perigee: | 266.5554° |
| revolutions per day: | 14.98334043 |
| mean anomaly at epoch: | 93.5170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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