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 33433U 26144.98193046 +.00000000 +00000-0 +56193-4 0 00004
2 33433 98.6076 171.7511 0013234 197.7305 162.3417 14.30793362 04
| Epoch (UTC): | 24 May 2026 23:33:58 |
| Eccentricity: | 0.0013234 |
| inclination: | 98.6076° |
| perigee height: | 780 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 171.7511° |
| argument of perigee: | 197.7305° |
| revolutions per day: | 14.30793362 |
| mean anomaly at epoch: | 162.3417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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