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 66244U 26145.38298983 +.00000000 +00000-0 +61777-3 0 00004
2 66244 53.1606 287.3035 0001277 94.5774 265.5372 15.30207782 01
| Epoch (UTC): | 25 May 2026 09:11:30 |
| Eccentricity: | 0.0001277 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.3035° |
| argument of perigee: | 94.5774° |
| revolutions per day: | 15.30207782 |
| mean anomaly at epoch: | 265.5372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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