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 33414U 26108.68595125 +.00000000 +00000-0 +00000-0 0 00006
2 33414 5.6084 73.7117 0063951 193.9721 3.4851 0.99274665 01
| Epoch (UTC): | 18 April 2026 16:27:46 |
| Eccentricity: | 0.0063951 |
| inclination: | 5.6084° |
| perigee height: | 35797 km |
| apogee height: | 36340 km |
| right ascension of ascending node: | 73.7117° |
| argument of perigee: | 193.9721° |
| revolutions per day: | 0.99274665 |
| mean anomaly at epoch: | 3.4851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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