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 56021U 26145.58432243 +.00000000 +00000-0 +81114-4 0 00005
2 56021 43.0051 331.1271 0002847 259.1402 100.9129 15.27581470 03
| Epoch (UTC): | 25 May 2026 14:01:25 |
| Eccentricity: | 0.0002847 |
| inclination: | 43.0051° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 331.1271° |
| argument of perigee: | 259.1402° |
| revolutions per day: | 15.27581470 |
| mean anomaly at epoch: | 100.9129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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