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 66970U 26145.47415073 +.00000000 +00000-0 +41689-3 0 00001
2 66970 43.0006 309.5501 0001728 273.3553 86.7101 15.27584915 02
| Epoch (UTC): | 25 May 2026 11:22:46 |
| Eccentricity: | 0.0001728 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.5501° |
| argument of perigee: | 273.3553° |
| revolutions per day: | 15.27584915 |
| mean anomaly at epoch: | 86.7101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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