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 00694U 26072.64775016 +.00000000 +00000-0 +26288-3 0 00004
2 00694 30.3515 173.5220 0547663 115.1616 250.6795 14.12083127 03
| Epoch (UTC): | 13 March 2026 15:32:45 |
| Eccentricity: | 0.0547663 |
| inclination: | 30.3515° |
| perigee height: | 456 km |
| apogee height: | 1248 km |
| right ascension of ascending node: | 173.5220° |
| argument of perigee: | 115.1616° |
| revolutions per day: | 14.12083127 |
| mean anomaly at epoch: | 250.6795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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