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 67741U 26145.11848472 +.00000000 +00000-0 +23411-3 0 00005
2 67741 97.2853 198.7160 0000879 92.8730 267.2613 15.33441193 07
| Epoch (UTC): | 25 May 2026 02:50:37 |
| Eccentricity: | 0.0000879 |
| inclination: | 97.2853° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.7160° |
| argument of perigee: | 92.8730° |
| revolutions per day: | 15.33441193 |
| mean anomaly at epoch: | 267.2613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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