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 66255U 26145.10390395 +.00000000 +00000-0 +75159-3 0 00005
2 66255 53.1578 289.1128 0001087 84.5150 275.5975 15.30202160 05
| Epoch (UTC): | 25 May 2026 02:29:37 |
| Eccentricity: | 0.0001087 |
| inclination: | 53.1578° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 289.1128° |
| argument of perigee: | 84.5150° |
| revolutions per day: | 15.30202160 |
| mean anomaly at epoch: | 275.5975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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