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 33274U 26145.61065948 +.00000000 +00000-0 +00000-0 0 00009
2 33274 2.3050 81.5328 0005694 16.2429 141.2483 1.00270616 02
| Epoch (UTC): | 25 May 2026 14:39:20 |
| Eccentricity: | 0.0005694 |
| inclination: | 2.3050° |
| perigee height: | 35763 km |
| apogee height: | 35811 km |
| right ascension of ascending node: | 81.5328° |
| argument of perigee: | 16.2429° |
| revolutions per day: | 1.00270616 |
| mean anomaly at epoch: | 141.2483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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