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 54694U 26145.61242358 +.00000000 +00000-0 +33690-3 0 00004
2 54694 97.6792 314.7248 0005234 203.5360 156.5645 15.36791617 00
| Epoch (UTC): | 25 May 2026 14:41:53 |
| Eccentricity: | 0.0005234 |
| inclination: | 97.6792° |
| perigee height: | 452 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 314.7248° |
| argument of perigee: | 203.5360° |
| revolutions per day: | 15.36791617 |
| mean anomaly at epoch: | 156.5645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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