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 67992U 26145.59284903 +.00000000 +00000-0 +48697-3 0 00001
2 67992 43.0030 334.7330 0001176 265.4085 94.6632 15.27594080 04
| Epoch (UTC): | 25 May 2026 14:13:42 |
| Eccentricity: | 0.0001176 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 334.7330° |
| argument of perigee: | 265.4085° |
| revolutions per day: | 15.27594080 |
| mean anomaly at epoch: | 94.6632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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