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 67999U 26145.55558222 +.00000000 +00000-0 +42313-3 0 00001
2 67999 43.0019 334.4385 0000609 293.4535 66.6253 15.27591225 02
| Epoch (UTC): | 25 May 2026 13:20:02 |
| Eccentricity: | 0.0000609 |
| inclination: | 43.0019° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 334.4385° |
| argument of perigee: | 293.4535° |
| revolutions per day: | 15.27591225 |
| mean anomaly at epoch: | 66.6253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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