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 67390U 26145.43625275 +.00000000 +00000-0 +13360-3 0 00006
2 67390 97.4586 144.7169 0005647 71.7400 288.4447 15.17734101 06
| Epoch (UTC): | 25 May 2026 10:28:12 |
| Eccentricity: | 0.0005647 |
| inclination: | 97.4586° |
| perigee height: | 509 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 144.7169° |
| argument of perigee: | 71.7400° |
| revolutions per day: | 15.17734101 |
| mean anomaly at epoch: | 288.4447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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