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 66095U 26145.15074340 +.00000000 +00000-0 +76001-3 0 00008
2 66095 53.1603 108.5362 0000925 111.5541 248.5559 15.30183034 01
| Epoch (UTC): | 25 May 2026 03:37:04 |
| Eccentricity: | 0.0000925 |
| inclination: | 53.1603° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.5362° |
| argument of perigee: | 111.5541° |
| revolutions per day: | 15.30183034 |
| mean anomaly at epoch: | 248.5559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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