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 67990U 26144.55309332 +.00000000 +00000-0 +53807-3 0 00007
2 67990 42.9988 340.6782 0001070 271.7911 88.2818 15.27586391 01
| Epoch (UTC): | 24 May 2026 13:16:27 |
| Eccentricity: | 0.0001070 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 340.6782° |
| argument of perigee: | 271.7911° |
| revolutions per day: | 15.27586391 |
| mean anomaly at epoch: | 88.2818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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