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 52581U 26145.24772715 +.00000000 +00000-0 +14957-3 0 00006
2 52581 53.2135 135.4382 0001176 83.8566 276.2560 15.08845350 06
| Epoch (UTC): | 25 May 2026 05:56:43 |
| Eccentricity: | 0.0001176 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 135.4382° |
| argument of perigee: | 83.8566° |
| revolutions per day: | 15.08845350 |
| mean anomaly at epoch: | 276.2560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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