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 66834U 26145.41743992 +.00000000 +00000-0 +24284-3 0 00000
2 66834 70.0009 140.8134 0004068 267.5340 92.5354 14.98337634 07
| Epoch (UTC): | 25 May 2026 10:01:06 |
| Eccentricity: | 0.0004068 |
| inclination: | 70.0009° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 140.8134° |
| argument of perigee: | 267.5340° |
| revolutions per day: | 14.98337634 |
| mean anomaly at epoch: | 92.5354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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