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 45154U 26145.46915786 +.00000000 +00000-0 +16916-2 0 00001
2 45154 87.8855 40.7991 0002110 89.5282 270.6087 13.10372354 09
| Epoch (UTC): | 25 May 2026 11:15:35 |
| Eccentricity: | 0.0002110 |
| inclination: | 87.8855° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7991° |
| argument of perigee: | 89.5282° |
| revolutions per day: | 13.10372354 |
| mean anomaly at epoch: | 270.6087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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