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 33373U 26145.56752169 +.00000000 +00000-0 +00000-0 0 00001
2 33373 0.0073 35.8471 0002028 23.0621 306.5748 1.00271120 02
| Epoch (UTC): | 25 May 2026 13:37:13 |
| Eccentricity: | 0.0002028 |
| inclination: | 0.0073° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 35.8471° |
| argument of perigee: | 23.0621° |
| revolutions per day: | 1.00271120 |
| mean anomaly at epoch: | 306.5748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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