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 66882U 26145.39544378 +.00000000 +00000-0 +86272-3 0 00002
2 66882 53.1605 27.4920 0001213 100.3071 259.8069 15.34409630 09
| Epoch (UTC): | 25 May 2026 09:29:26 |
| Eccentricity: | 0.0001213 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 27.4920° |
| argument of perigee: | 100.3071° |
| revolutions per day: | 15.34409630 |
| mean anomaly at epoch: | 259.8069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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