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 45456U 26145.64423811 +.00000000 +00000-0 +10274-2 0 00000
2 45456 87.8921 25.5455 0001608 56.7175 303.4107 13.11417563 03
| Epoch (UTC): | 25 May 2026 15:27:42 |
| Eccentricity: | 0.0001608 |
| inclination: | 87.8921° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5455° |
| argument of perigee: | 56.7175° |
| revolutions per day: | 13.11417563 |
| mean anomaly at epoch: | 303.4107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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