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 56474U 26145.38791399 +.00000000 +00000-0 -35248-5 0 00004
2 56474 69.9988 291.2435 0003018 269.3669 90.7145 14.98327471 08
| Epoch (UTC): | 25 May 2026 09:18:35 |
| Eccentricity: | 0.0003018 |
| inclination: | 69.9988° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 291.2435° |
| argument of perigee: | 269.3669° |
| revolutions per day: | 14.98327471 |
| mean anomaly at epoch: | 90.7145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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