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 67713U 26145.27418181 +.00000000 +00000-0 +63277-3 0 00005
2 67713 97.2820 256.0349 0001333 129.9702 230.1658 15.33458829 06
| Epoch (UTC): | 25 May 2026 06:34:49 |
| Eccentricity: | 0.0001333 |
| inclination: | 97.2820° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 256.0349° |
| argument of perigee: | 129.9702° |
| revolutions per day: | 15.33458829 |
| mean anomaly at epoch: | 230.1658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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