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 45320U 26088.18796382 +.00000000 +00000-0 +16200-2 0 00006
2 45320 82.5673 148.3493 0083807 85.1619 275.9077 13.36918002 05
| Epoch (UTC): | 29 March 2026 04:30:40 |
| Eccentricity: | 0.0083807 |
| inclination: | 82.5673° |
| perigee height: | 1058 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 148.3493° |
| argument of perigee: | 85.1619° |
| revolutions per day: | 13.36918002 |
| mean anomaly at epoch: | 275.9077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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