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 52303U 26145.63229544 +.00000000 +00000-0 +37728-3 0 00009
2 52303 53.2139 113.7105 0001261 86.3613 273.7524 15.08818808 00
| Epoch (UTC): | 25 May 2026 15:10:30 |
| Eccentricity: | 0.0001261 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 113.7105° |
| argument of perigee: | 86.3613° |
| revolutions per day: | 15.08818808 |
| mean anomaly at epoch: | 273.7524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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