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 26088.12770888 +.00000000 +00000-0 +58492-3 0 00006
2 33498 98.1483 32.2383 0010358 76.7900 283.4474 14.95130905 08
| Epoch (UTC): | 29 March 2026 03:03:54 |
| Eccentricity: | 0.0010358 |
| inclination: | 98.1483° |
| perigee height: | 575 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 32.2383° |
| argument of perigee: | 76.7900° |
| revolutions per day: | 14.95130905 |
| mean anomaly at epoch: | 283.4474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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