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 67734U 26145.14295784 +.00000000 +00000-0 +62441-3 0 00008
2 67734 97.2860 198.6827 0000370 125.3338 234.7940 15.33443570 01
| Epoch (UTC): | 25 May 2026 03:25:51 |
| Eccentricity: | 0.0000370 |
| inclination: | 97.2860° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.6827° |
| argument of perigee: | 125.3338° |
| revolutions per day: | 15.33443570 |
| mean anomaly at epoch: | 234.7940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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