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 52306U 26145.61113083 +.00000000 +00000-0 +51589-4 0 00002
2 52306 53.2131 103.8065 0001095 108.5563 251.5548 15.08843822 00
| Epoch (UTC): | 25 May 2026 14:40:01 |
| Eccentricity: | 0.0001095 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 103.8065° |
| argument of perigee: | 108.5563° |
| revolutions per day: | 15.08843822 |
| mean anomaly at epoch: | 251.5548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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