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 33496U 26141.22194201 +.00000000 +00000-0 +50239-4 0 00006
2 33496 98.1418 45.7948 0007235 99.1930 261.0097 14.74994555 01
| Epoch (UTC): | 21 May 2026 05:19:35 |
| Eccentricity: | 0.0007235 |
| inclination: | 98.1418° |
| perigee height: | 640 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 45.7948° |
| argument of perigee: | 99.1930° |
| revolutions per day: | 14.74994555 |
| mean anomaly at epoch: | 261.0097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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