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 45172U 26105.39841828 +.00000000 +00000-0 +86294-2 0 00000
2 45172 82.4664 151.3588 0084006 280.8694 78.2955 12.68271681 05
| Epoch (UTC): | 15 April 2026 09:33:43 |
| Eccentricity: | 0.0084006 |
| inclination: | 82.4664° |
| perigee height: | 1324 km |
| apogee height: | 1454 km |
| right ascension of ascending node: | 151.3588° |
| argument of perigee: | 280.8694° |
| revolutions per day: | 12.68271681 |
| mean anomaly at epoch: | 78.2955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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