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 33497U 26150.30649721 +.00000000 +00000-0 +13130-3 0 00006
2 33497 98.1935 49.3132 0002031 22.9128 337.2170 14.74496819 01
| Epoch (UTC): | 30 May 2026 07:21:21 |
| Eccentricity: | 0.0002031 |
| inclination: | 98.1935° |
| perigee height: | 645 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 49.3132° |
| argument of perigee: | 22.9128° |
| revolutions per day: | 14.74496819 |
| mean anomaly at epoch: | 337.2170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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