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 33207U 26145.56197500 +.00000000 +00000-0 +00000-0 0 00009
2 33207 0.9487 84.4143 0002473 324.4419 286.8017 1.00272354 08
| Epoch (UTC): | 25 May 2026 13:29:14 |
| Eccentricity: | 0.0002473 |
| inclination: | 0.9487° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 84.4143° |
| argument of perigee: | 324.4419° |
| revolutions per day: | 1.00272354 |
| mean anomaly at epoch: | 286.8017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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