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 56525U 26145.66668980 +.00000000 +00000-0 +48907-3 0 00004
2 56525 43.0002 148.2212 0001615 307.2743 258.2187 15.21231179 08
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001615 |
| inclination: | 43.0002° |
| perigee height: | 501 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 148.2212° |
| argument of perigee: | 307.2743° |
| revolutions per day: | 15.21231179 |
| mean anomaly at epoch: | 258.2187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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