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 26074.27360955 +.00000000 +00000-0 +45686-3 0 00008
2 33498 98.1468 17.8503 0010022 113.9806 246.2464 14.95005769 06
| Epoch (UTC): | 15 March 2026 06:33:59 |
| Eccentricity: | 0.0010022 |
| inclination: | 98.1468° |
| perigee height: | 575 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 17.8503° |
| argument of perigee: | 113.9806° |
| revolutions per day: | 14.95005769 |
| mean anomaly at epoch: | 246.2464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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