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 26071.39557051 +.00000000 +00000-0 +55682-3 0 00000
2 33498 98.1463 14.8625 0009992 122.4143 237.8044 14.94973807 02
| Epoch (UTC): | 12 March 2026 09:29:37 |
| Eccentricity: | 0.0009992 |
| inclination: | 98.1463° |
| perigee height: | 575 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 14.8625° |
| argument of perigee: | 122.4143° |
| revolutions per day: | 14.94973807 |
| mean anomaly at epoch: | 237.8044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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