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 56387U 26145.33187250 +.00000000 +00000-0 +26534-4 0 00003
2 56387 43.0051 124.8430 0001490 285.8782 74.1905 15.27578262 01
| Epoch (UTC): | 25 May 2026 07:57:53 |
| Eccentricity: | 0.0001490 |
| inclination: | 43.0051° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.8430° |
| argument of perigee: | 285.8782° |
| revolutions per day: | 15.27578262 |
| mean anomaly at epoch: | 74.1905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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