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 52559U 26145.36918677 +.00000000 +00000-0 +13743-5 0 00007
2 52559 53.2128 135.0757 0000902 106.7802 253.3290 15.08844573 01
| Epoch (UTC): | 25 May 2026 08:51:37 |
| Eccentricity: | 0.0000902 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 135.0757° |
| argument of perigee: | 106.7802° |
| revolutions per day: | 15.08844573 |
| mean anomaly at epoch: | 253.3290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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