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 56131U 26145.15365041 +.00000000 +00000-0 +89282-4 0 00005
2 56131 43.0030 75.2113 0001299 268.3903 91.6800 15.27571066 03
| Epoch (UTC): | 25 May 2026 03:41:15 |
| Eccentricity: | 0.0001299 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 75.2113° |
| argument of perigee: | 268.3903° |
| revolutions per day: | 15.27571066 |
| mean anomaly at epoch: | 91.6800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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