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 56494U 26145.40034640 +.00000000 +00000-0 +13732-4 0 00000
2 56494 69.9992 271.0117 0003189 267.7458 92.3335 14.98330994 08
| Epoch (UTC): | 25 May 2026 09:36:29 |
| Eccentricity: | 0.0003189 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 271.0117° |
| argument of perigee: | 267.7458° |
| revolutions per day: | 14.98330994 |
| mean anomaly at epoch: | 92.3335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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