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 66749U 26145.63370154 +.00000000 +00000-0 +24834-3 0 00006
2 66749 97.4197 219.6547 0003697 68.3215 291.8413 15.19988847 03
| Epoch (UTC): | 25 May 2026 15:12:31 |
| Eccentricity: | 0.0003697 |
| inclination: | 97.4197° |
| perigee height: | 503 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 219.6547° |
| argument of perigee: | 68.3215° |
| revolutions per day: | 15.19988847 |
| mean anomaly at epoch: | 291.8413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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