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 66711U 26145.14347663 +.00000000 +00000-0 +30718-3 0 00008
2 66711 97.4230 219.1678 0005155 97.6837 262.4984 15.19820148 02
| Epoch (UTC): | 25 May 2026 03:26:36 |
| Eccentricity: | 0.0005155 |
| inclination: | 97.4230° |
| perigee height: | 503 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 219.1678° |
| argument of perigee: | 97.6837° |
| revolutions per day: | 15.19820148 |
| mean anomaly at epoch: | 262.4984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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