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 26474U 26065.25109267 +.00000000 +00000-0 +34026-3 0 00005
2 26474 67.9893 50.1787 0038272 39.4556 320.9368 15.09520809 09
| Epoch (UTC): | 06 March 2026 06:01:34 |
| Eccentricity: | 0.0038272 |
| inclination: | 67.9893° |
| perigee height: | 511 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 50.1787° |
| argument of perigee: | 39.4556° |
| revolutions per day: | 15.09520809 |
| mean anomaly at epoch: | 320.9368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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