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 26145.40578208 +.00000000 +00000-0 +36453-3 0 00006
2 33498 98.1542 91.7893 0006669 239.7078 120.3482 14.95568140 01
| Epoch (UTC): | 25 May 2026 09:44:19 |
| Eccentricity: | 0.0006669 |
| inclination: | 98.1542° |
| perigee height: | 576 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 91.7893° |
| argument of perigee: | 239.7078° |
| revolutions per day: | 14.95568140 |
| mean anomaly at epoch: | 120.3482° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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