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 53409U 26145.34665020 +.00000000 +00000-0 +15004-6 0 00004
2 53409 53.2124 120.1873 0001334 81.2947 278.8196 15.08834922 07
| Epoch (UTC): | 25 May 2026 08:19:10 |
| Eccentricity: | 0.0001334 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 120.1873° |
| argument of perigee: | 81.2947° |
| revolutions per day: | 15.08834922 |
| mean anomaly at epoch: | 278.8196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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