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 56049U 26145.53918713 +.00000000 +00000-0 -19621-3 0 00005
2 56049 87.9253 248.4794 0001792 100.7389 259.3947 13.21825791 03
| Epoch (UTC): | 25 May 2026 12:56:25 |
| Eccentricity: | 0.0001792 |
| inclination: | 87.9253° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4794° |
| argument of perigee: | 100.7389° |
| revolutions per day: | 13.21825791 |
| mean anomaly at epoch: | 259.3947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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