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 56496U 26145.38765986 +.00000000 +00000-0 +27167-4 0 00000
2 56496 69.9992 270.9672 0003675 267.7897 92.2841 14.98329114 04
| Epoch (UTC): | 25 May 2026 09:18:13 |
| Eccentricity: | 0.0003675 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 270.9672° |
| argument of perigee: | 267.7897° |
| revolutions per day: | 14.98329114 |
| mean anomaly at epoch: | 92.2841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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