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 33060U 26088.19976263 +.00000000 +00000-0 +37164-3 0 00006
2 33060 48.4404 35.4672 0004532 196.6151 163.4617 14.82818461 09
| Epoch (UTC): | 29 March 2026 04:47:39 |
| Eccentricity: | 0.0004532 |
| inclination: | 48.4404° |
| perigee height: | 617 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 35.4672° |
| argument of perigee: | 196.6151° |
| revolutions per day: | 14.82818461 |
| mean anomaly at epoch: | 163.4617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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