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 56134U 26145.52026731 +.00000000 +00000-0 +14442-4 0 00005
2 56134 43.0065 72.8082 0001433 271.9072 88.1615 15.27575956 06
| Epoch (UTC): | 25 May 2026 12:29:11 |
| Eccentricity: | 0.0001433 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 72.8082° |
| argument of perigee: | 271.9072° |
| revolutions per day: | 15.27575956 |
| mean anomaly at epoch: | 88.1615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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