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 56353U 26145.26411936 +.00000000 +00000-0 -71619-4 0 00004
2 56353 97.4466 145.1839 0004063 107.2146 252.9527 15.05652541 01
| Epoch (UTC): | 25 May 2026 06:20:19 |
| Eccentricity: | 0.0004063 |
| inclination: | 97.4466° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 145.1839° |
| argument of perigee: | 107.2146° |
| revolutions per day: | 15.05652541 |
| mean anomaly at epoch: | 252.9527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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