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 56001U 26145.60132039 +.00000000 +00000-0 +27747-4 0 00008
2 56001 43.0021 349.3808 0001102 268.6474 91.4252 15.27578882 06
| Epoch (UTC): | 25 May 2026 14:25:54 |
| Eccentricity: | 0.0001102 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 349.3808° |
| argument of perigee: | 268.6474° |
| revolutions per day: | 15.27578882 |
| mean anomaly at epoch: | 91.4252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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