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 66275U 26145.57447774 +.00000000 +00000-0 +39450-3 0 00006
2 66275 53.1578 194.4247 0001452 39.8435 320.2672 15.30208461 04
| Epoch (UTC): | 25 May 2026 13:47:14 |
| Eccentricity: | 0.0001452 |
| inclination: | 53.1578° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 194.4247° |
| argument of perigee: | 39.8435° |
| revolutions per day: | 15.30208461 |
| mean anomaly at epoch: | 320.2672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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