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 56793U 26145.41965642 +.00000000 +00000-0 +30862-4 0 00001
2 56793 69.9983 150.9924 0003801 266.7580 93.3144 14.98329940 05
| Epoch (UTC): | 25 May 2026 10:04:18 |
| Eccentricity: | 0.0003801 |
| inclination: | 69.9983° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 150.9924° |
| argument of perigee: | 266.7580° |
| revolutions per day: | 14.98329940 |
| mean anomaly at epoch: | 93.3144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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