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 00045U 26131.31530818 +.00000000 +00000-0 +33058-4 0 00007
2 00045 66.6920 97.7237 0249584 187.8078 171.9110 14.35945741 09
| Epoch (UTC): | 11 May 2026 07:34:02 |
| Eccentricity: | 0.0249584 |
| inclination: | 66.6920° |
| perigee height: | 593 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 97.7237° |
| argument of perigee: | 187.8078° |
| revolutions per day: | 14.35945741 |
| mean anomaly at epoch: | 171.9110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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