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 49332U 26145.57046838 +.00000000 +00000-0 +00000-0 0 00003
2 49332 0.0323 44.4135 0001033 16.1211 320.8898 1.00269644 01
| Epoch (UTC): | 25 May 2026 13:41:28 |
| Eccentricity: | 0.0001033 |
| inclination: | 0.0323° |
| perigee height: | 35783 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 44.4135° |
| argument of perigee: | 16.1211° |
| revolutions per day: | 1.00269644 |
| mean anomaly at epoch: | 320.8898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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