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 56067U 26145.54510133 +.00000000 +00000-0 +34675-3 0 00005
2 56067 87.9257 248.4768 0002225 106.5355 253.6024 13.21825716 07
| Epoch (UTC): | 25 May 2026 13:04:56 |
| Eccentricity: | 0.0002225 |
| inclination: | 87.9257° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4768° |
| argument of perigee: | 106.5355° |
| revolutions per day: | 13.21825716 |
| mean anomaly at epoch: | 253.6024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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