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 45080U 26145.03478831 +.00000000 +00000-0 +11991-2 0 00005
2 45080 53.1587 261.7843 0003809 279.4184 80.6389 15.36031161 05
| Epoch (UTC): | 25 May 2026 00:50:05 |
| Eccentricity: | 0.0003809 |
| inclination: | 53.1587° |
| perigee height: | 455 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 261.7843° |
| argument of perigee: | 279.4184° |
| revolutions per day: | 15.36031161 |
| mean anomaly at epoch: | 80.6389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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