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 56073U 26145.58046470 +.00000000 +00000-0 -44977-3 0 00001
2 56073 87.8992 263.7180 0002035 96.5588 263.5774 13.15548693 03
| Epoch (UTC): | 25 May 2026 13:55:52 |
| Eccentricity: | 0.0002035 |
| inclination: | 87.8992° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7180° |
| argument of perigee: | 96.5588° |
| revolutions per day: | 13.15548693 |
| mean anomaly at epoch: | 263.5774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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