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 66770U 26145.63628515 +.00000000 +00000-0 +98068-4 0 00008
2 66770 97.4249 219.7688 0001793 25.1604 334.9718 15.19387575 08
| Epoch (UTC): | 25 May 2026 15:16:15 |
| Eccentricity: | 0.0001793 |
| inclination: | 97.4249° |
| perigee height: | 506 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 219.7688° |
| argument of perigee: | 25.1604° |
| revolutions per day: | 15.19387575 |
| mean anomaly at epoch: | 334.9718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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