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 33055U 26145.58017508 +.00000000 +00000-0 +00000-0 0 00001
2 33055 3.7335 77.3014 0004018 352.7052 4.2517 1.00271735 03
| Epoch (UTC): | 25 May 2026 13:55:27 |
| Eccentricity: | 0.0004018 |
| inclination: | 3.7335° |
| perigee height: | 35770 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 77.3014° |
| argument of perigee: | 352.7052° |
| revolutions per day: | 1.00271735 |
| mean anomaly at epoch: | 4.2517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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