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 45670U 26145.61369237 +.00000000 +00000-0 +54724-3 0 00005
2 45670 53.0413 358.1738 0002236 150.9135 209.2005 15.66772270 03
| Epoch (UTC): | 25 May 2026 14:43:43 |
| Eccentricity: | 0.0002236 |
| inclination: | 53.0413° |
| perigee height: | 367 km |
| apogee height: | 370 km |
| right ascension of ascending node: | 358.1738° |
| argument of perigee: | 150.9135° |
| revolutions per day: | 15.66772270 |
| mean anomaly at epoch: | 209.2005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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