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 66094U 26145.21920468 +.00000000 +00000-0 -15095-3 0 00002
2 66094 53.1592 108.2545 0001255 118.3703 241.7424 15.30218193 00
| Epoch (UTC): | 25 May 2026 05:15:39 |
| Eccentricity: | 0.0001255 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.2545° |
| argument of perigee: | 118.3703° |
| revolutions per day: | 15.30218193 |
| mean anomaly at epoch: | 241.7424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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