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 26106.26051741 +.00000000 +00000-0 +10378-3 0 00009
2 26474 67.9868 294.8361 0041437 352.0404 8.0082 15.09869384 00
| Epoch (UTC): | 16 April 2026 06:15:08 |
| Eccentricity: | 0.0041437 |
| inclination: | 67.9868° |
| perigee height: | 508 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 294.8361° |
| argument of perigee: | 352.0404° |
| revolutions per day: | 15.09869384 |
| mean anomaly at epoch: | 8.0082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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