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 26102.24797080 +.00000000 +00000-0 +28474-3 0 00006
2 33498 98.1493 46.9102 0009319 37.1771 323.0092 14.95288341 07
| Epoch (UTC): | 12 April 2026 05:57:04 |
| Eccentricity: | 0.0009319 |
| inclination: | 98.1493° |
| perigee height: | 575 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 46.9102° |
| argument of perigee: | 37.1771° |
| revolutions per day: | 14.95288341 |
| mean anomaly at epoch: | 323.0092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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