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 66009U 26145.61533568 +.00000000 +00000-0 +60893-3 0 00008
2 66009 53.1609 106.5667 0001502 96.1310 263.9862 15.30204065 08
| Epoch (UTC): | 25 May 2026 14:46:05 |
| Eccentricity: | 0.0001502 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.5667° |
| argument of perigee: | 96.1310° |
| revolutions per day: | 15.30204065 |
| mean anomaly at epoch: | 263.9862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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