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 56004U 26145.61917007 +.00000000 +00000-0 -77561-4 0 00008
2 56004 43.0066 348.6610 0001760 263.4219 96.6433 15.27568719 07
| Epoch (UTC): | 25 May 2026 14:51:36 |
| Eccentricity: | 0.0001760 |
| inclination: | 43.0066° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 348.6610° |
| argument of perigee: | 263.4219° |
| revolutions per day: | 15.27568719 |
| mean anomaly at epoch: | 96.6433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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