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 56808U 26145.24152023 +.00000000 +00000-0 +39409-4 0 00006
2 56808 69.9998 81.5254 0002856 265.5028 94.5805 14.98332014 09
| Epoch (UTC): | 25 May 2026 05:47:47 |
| Eccentricity: | 0.0002856 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.5254° |
| argument of perigee: | 265.5028° |
| revolutions per day: | 14.98332014 |
| mean anomaly at epoch: | 94.5805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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