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 33105U 26150.24634649 +.00000000 +00000-0 -75467-4 0 00001
2 33105 66.0397 88.5717 0008010 270.9582 195.9231 12.87697311 08
| Epoch (UTC): | 30 May 2026 05:54:44 |
| Eccentricity: | 0.0008010 |
| inclination: | 66.0397° |
| perigee height: | 1305 km |
| apogee height: | 1317 km |
| right ascension of ascending node: | 88.5717° |
| argument of perigee: | 270.9582° |
| revolutions per day: | 12.87697311 |
| mean anomaly at epoch: | 195.9231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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