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 53318U 26145.65607894 +.00000000 +00000-0 +33082-3 0 00005
2 53318 34.9896 350.7753 0011620 182.4478 177.6182 15.24407986 03
| Epoch (UTC): | 25 May 2026 15:44:45 |
| Eccentricity: | 0.0011620 |
| inclination: | 34.9896° |
| perigee height: | 485 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 350.7753° |
| argument of perigee: | 182.4478° |
| revolutions per day: | 15.24407986 |
| mean anomaly at epoch: | 177.6182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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