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 56895U 26145.04424368 +.00000000 +00000-0 -77836-4 0 00001
2 56895 43.0052 17.7526 0001653 250.4999 109.5674 15.27573977 05
| Epoch (UTC): | 25 May 2026 01:03:42 |
| Eccentricity: | 0.0001653 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 17.7526° |
| argument of perigee: | 250.4999° |
| revolutions per day: | 15.27573977 |
| mean anomaly at epoch: | 109.5674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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