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 67914U 26145.44779247 +.00000000 +00000-0 +38293-3 0 00000
2 67914 43.0016 171.5605 0001381 265.0857 94.9837 15.27592145 05
| Epoch (UTC): | 25 May 2026 10:44:49 |
| Eccentricity: | 0.0001381 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.5605° |
| argument of perigee: | 265.0857° |
| revolutions per day: | 15.27592145 |
| mean anomaly at epoch: | 94.9837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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