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 26071.94315221 +.00000000 +00000-0 +31822-3 0 00008
2 26474 67.9903 31.3612 0038674 31.5697 328.7761 15.09598814 08
| Epoch (UTC): | 12 March 2026 22:38:08 |
| Eccentricity: | 0.0038674 |
| inclination: | 67.9903° |
| perigee height: | 511 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 31.3612° |
| argument of perigee: | 31.5697° |
| revolutions per day: | 15.09598814 |
| mean anomaly at epoch: | 328.7761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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