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 26075.07677294 +.00000000 +00000-0 +31882-3 0 00007
2 33498 98.1470 18.6841 0009969 111.8534 248.3747 14.95010958 09
| Epoch (UTC): | 16 March 2026 01:50:33 |
| Eccentricity: | 0.0009969 |
| inclination: | 98.1470° |
| perigee height: | 575 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 18.6841° |
| argument of perigee: | 111.8534° |
| revolutions per day: | 14.95010958 |
| mean anomaly at epoch: | 248.3747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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