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 49333U 26144.73719066 +.00000000 +00000-0 +00000-0 0 00001
2 49333 0.0114 335.8092 0001482 84.9093 132.4993 1.00271121 04
| Epoch (UTC): | 24 May 2026 17:41:33 |
| Eccentricity: | 0.0001482 |
| inclination: | 0.0114° |
| perigee height: | 35781 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 335.8092° |
| argument of perigee: | 84.9093° |
| revolutions per day: | 1.00271121 |
| mean anomaly at epoch: | 132.4993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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