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 66838U 26145.36337824 +.00000000 +00000-0 -81871-4 0 00008
2 66838 70.0007 141.0216 0003657 268.6303 91.4437 14.98321335 08
| Epoch (UTC): | 25 May 2026 08:43:15 |
| Eccentricity: | 0.0003657 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.0216° |
| argument of perigee: | 268.6303° |
| revolutions per day: | 14.98321335 |
| mean anomaly at epoch: | 91.4437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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