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 33053U 26151.53119558 +.00000000 +00000-0 +16853-3 0 00005
2 33053 25.5837 320.1254 0008578 127.5054 232.6265 15.23848488 02
| Epoch (UTC): | 31 May 2026 12:44:55 |
| Eccentricity: | 0.0008578 |
| inclination: | 25.5837° |
| perigee height: | 488 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 320.1254° |
| argument of perigee: | 127.5054° |
| revolutions per day: | 15.23848488 |
| mean anomaly at epoch: | 232.6265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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