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 67905U 26145.36071316 +.00000000 +00000-0 +54895-3 0 00009
2 67905 42.9971 172.6458 0000711 260.5053 99.5719 15.27593247 09
| Epoch (UTC): | 25 May 2026 08:39:25 |
| Eccentricity: | 0.0000711 |
| inclination: | 42.9971° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 172.6458° |
| argument of perigee: | 260.5053° |
| revolutions per day: | 15.27593247 |
| mean anomaly at epoch: | 99.5719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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