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 56467U 26145.11252185 +.00000000 +00000-0 +67929-8 0 00005
2 56467 69.9991 291.8877 0002862 270.7560 89.3271 14.98331934 05
| Epoch (UTC): | 25 May 2026 02:42:01 |
| Eccentricity: | 0.0002862 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 291.8877° |
| argument of perigee: | 270.7560° |
| revolutions per day: | 14.98331934 |
| mean anomaly at epoch: | 89.3271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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