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 66393U 26145.59774419 +.00000000 +00000-0 +44555-3 0 00000
2 66393 53.1598 220.1318 0001048 102.9729 257.1389 15.30207222 09
| Epoch (UTC): | 25 May 2026 14:20:45 |
| Eccentricity: | 0.0001048 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 220.1318° |
| argument of perigee: | 102.9729° |
| revolutions per day: | 15.30207222 |
| mean anomaly at epoch: | 257.1389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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