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 67991U 26144.94284536 +.00000000 +00000-0 +54271-3 0 00005
2 67991 43.0027 338.4649 0001494 274.4559 85.6121 15.27587006 05
| Epoch (UTC): | 24 May 2026 22:37:41 |
| Eccentricity: | 0.0001494 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.4649° |
| argument of perigee: | 274.4559° |
| revolutions per day: | 15.27587006 |
| mean anomaly at epoch: | 85.6121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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