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 56023U 26145.20999876 +.00000000 +00000-0 +32346-4 0 00009
2 56023 43.0018 333.4698 0001228 261.7601 98.3111 15.27587851 08
| Epoch (UTC): | 25 May 2026 05:02:23 |
| Eccentricity: | 0.0001228 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 333.4698° |
| argument of perigee: | 261.7601° |
| revolutions per day: | 15.27587851 |
| mean anomaly at epoch: | 98.3111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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