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 33494U 26150.30627834 +.00000000 +00000-0 +12268-3 0 00005
2 33494 98.1535 55.1731 0004733 67.3689 292.8020 14.75333985 05
| Epoch (UTC): | 30 May 2026 07:21:02 |
| Eccentricity: | 0.0004733 |
| inclination: | 98.1535° |
| perigee height: | 641 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 55.1731° |
| argument of perigee: | 67.3689° |
| revolutions per day: | 14.75333985 |
| mean anomaly at epoch: | 292.8020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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