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 52302U 26145.28728287 +.00000000 +00000-0 +38793-4 0 00001
2 52302 53.2137 105.2592 0001081 83.6025 276.5090 15.08845042 09
| Epoch (UTC): | 25 May 2026 06:53:41 |
| Eccentricity: | 0.0001081 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 105.2592° |
| argument of perigee: | 83.6025° |
| revolutions per day: | 15.08845042 |
| mean anomaly at epoch: | 276.5090° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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