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 66296U 26145.56638839 +.00000000 +00000-0 +25500-3 0 00003
2 66296 45.4041 241.8153 0006600 289.0847 70.9325 15.21353316 09
| Epoch (UTC): | 25 May 2026 13:35:35 |
| Eccentricity: | 0.0006600 |
| inclination: | 45.4041° |
| perigee height: | 497 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 241.8153° |
| argument of perigee: | 289.0847° |
| revolutions per day: | 15.21353316 |
| mean anomaly at epoch: | 70.9325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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