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 32253U 26145.55703498 +.00000000 +00000-0 +00000-0 0 00007
2 32253 3.5088 78.9347 0000795 80.7809 149.1816 0.99049115 00
| Epoch (UTC): | 25 May 2026 13:22:07 |
| Eccentricity: | 0.0000795 |
| inclination: | 3.5088° |
| perigee height: | 36130 km |
| apogee height: | 36136 km |
| right ascension of ascending node: | 78.9347° |
| argument of perigee: | 80.7809° |
| revolutions per day: | 0.99049115 |
| mean anomaly at epoch: | 149.1816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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