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 26073.26965000 +.00000000 +00000-0 +49819-3 0 00000
2 33498 98.1467 16.8080 0010006 116.8727 243.3517 14.94994609 06
| Epoch (UTC): | 14 March 2026 06:28:17 |
| Eccentricity: | 0.0010006 |
| inclination: | 98.1467° |
| perigee height: | 575 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 16.8080° |
| argument of perigee: | 116.8727° |
| revolutions per day: | 14.94994609 |
| mean anomaly at epoch: | 243.3517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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