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 66128U 26145.40712634 +.00000000 +00000-0 +19369-2 0 00001
2 66128 53.1583 43.4666 0000970 48.1773 311.9311 15.30194461 08
| Epoch (UTC): | 25 May 2026 09:46:15 |
| Eccentricity: | 0.0000970 |
| inclination: | 53.1583° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.4666° |
| argument of perigee: | 48.1773° |
| revolutions per day: | 15.30194461 |
| mean anomaly at epoch: | 311.9311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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