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 66315U 26145.46984997 +.00000000 +00000-0 +91933-4 0 00007
2 66315 98.1825 153.1497 0001341 88.8882 271.2471 14.59198849 09
| Epoch (UTC): | 25 May 2026 11:16:35 |
| Eccentricity: | 0.0001341 |
| inclination: | 98.1825° |
| perigee height: | 695 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 153.1497° |
| argument of perigee: | 88.8882° |
| revolutions per day: | 14.59198849 |
| mean anomaly at epoch: | 271.2471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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