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 52708U 26145.27762277 +.00000000 +00000-0 +91809-4 0 00004
2 52708 53.2137 150.2912 0000988 85.9528 274.1577 15.08841391 00
| Epoch (UTC): | 25 May 2026 06:39:46 |
| Eccentricity: | 0.0000988 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 150.2912° |
| argument of perigee: | 85.9528° |
| revolutions per day: | 15.08841391 |
| mean anomaly at epoch: | 274.1577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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