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 33498U 26150.82501757 +.00000000 +00000-0 +38175-3 0 00006
2 33498 98.1547 97.4281 0007183 220.1963 139.8726 14.95618619 02
| Epoch (UTC): | 30 May 2026 19:48:01 |
| Eccentricity: | 0.0007183 |
| inclination: | 98.1547° |
| perigee height: | 575 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 97.4281° |
| argument of perigee: | 220.1963° |
| revolutions per day: | 14.95618619 |
| mean anomaly at epoch: | 139.8726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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