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 26064.80027147 +.00000000 +00000-0 +22416-3 0 00007
2 00694 30.3516 217.3796 0547771 46.0087 318.4365 14.12053945 04
| Epoch (UTC): | 05 March 2026 19:12:23 |
| Eccentricity: | 0.0547771 |
| inclination: | 30.3516° |
| perigee height: | 456 km |
| apogee height: | 1248 km |
| right ascension of ascending node: | 217.3796° |
| argument of perigee: | 46.0087° |
| revolutions per day: | 14.12053945 |
| mean anomaly at epoch: | 318.4365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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