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 33062U 26088.12814308 +.00000000 +00000-0 +31703-3 0 00005
2 33062 48.4385 52.0127 0005196 178.1504 274.0241 14.82522104 01
| Epoch (UTC): | 29 March 2026 03:04:31 |
| Eccentricity: | 0.0005196 |
| inclination: | 48.4385° |
| perigee height: | 618 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 52.0127° |
| argument of perigee: | 178.1504° |
| revolutions per day: | 14.82522104 |
| mean anomaly at epoch: | 274.0241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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