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 52551U 26145.37928830 +.00000000 +00000-0 -10157-5 0 00009
2 52551 53.2129 144.8472 0000973 71.9429 288.1669 15.08842012 04
| Epoch (UTC): | 25 May 2026 09:06:10 |
| Eccentricity: | 0.0000973 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 144.8472° |
| argument of perigee: | 71.9429° |
| revolutions per day: | 15.08842012 |
| mean anomaly at epoch: | 288.1669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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