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 66066U 26145.01161086 +.00000000 +00000-0 +42993-3 0 00008
2 66066 53.1624 250.9765 0000870 97.9798 262.1302 15.30207825 04
| Epoch (UTC): | 25 May 2026 00:16:43 |
| Eccentricity: | 0.0000870 |
| inclination: | 53.1624° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 250.9765° |
| argument of perigee: | 97.9798° |
| revolutions per day: | 15.30207825 |
| mean anomaly at epoch: | 262.1302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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