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 66698U 26145.10681737 +.00000000 +00000-0 +24974-3 0 00008
2 66698 97.4188 218.9675 0005714 91.6179 268.5710 15.19444921 01
| Epoch (UTC): | 25 May 2026 02:33:49 |
| Eccentricity: | 0.0005714 |
| inclination: | 97.4188° |
| perigee height: | 504 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 218.9675° |
| argument of perigee: | 91.6179° |
| revolutions per day: | 15.19444921 |
| mean anomaly at epoch: | 268.5710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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