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 66828U 26145.33401074 +.00000000 +00000-0 +30038-3 0 00000
2 66828 70.0006 141.3235 0003903 265.1403 94.9311 14.98338164 04
| Epoch (UTC): | 25 May 2026 08:00:58 |
| Eccentricity: | 0.0003903 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.3235° |
| argument of perigee: | 265.1403° |
| revolutions per day: | 14.98338164 |
| mean anomaly at epoch: | 94.9311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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