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 67385U 26145.25724552 +.00000000 +00000-0 +18219-3 0 00006
2 67385 97.8000 144.1999 0001640 91.7295 268.4108 14.86631343 04
| Epoch (UTC): | 25 May 2026 06:10:26 |
| Eccentricity: | 0.0001640 |
| inclination: | 97.8000° |
| perigee height: | 607 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 144.1999° |
| argument of perigee: | 91.7295° |
| revolutions per day: | 14.86631343 |
| mean anomaly at epoch: | 268.4108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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