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 00005U 26104.81673522 +.00000000 +00000-0 +15153-3 0 00003
2 00005 34.2471 149.8755 1836480 212.7806 134.4457 10.85970086 05
| Epoch (UTC): | 14 April 2026 19:36:05 |
| Eccentricity: | 0.1836480 |
| inclination: | 34.2471° |
| perigee height: | 654 km |
| apogee height: | 3817 km |
| right ascension of ascending node: | 149.8755° |
| argument of perigee: | 212.7806° |
| revolutions per day: | 10.85970086 |
| mean anomaly at epoch: | 134.4457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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