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 04014U 26073.90882741 +.00000000 +00000-0 +23704-2 0 00007
2 04014 67.6275 35.1920 0815213 47.0407 348.0216 12.30149922 03
| Epoch (UTC): | 14 March 2026 21:48:42 |
| Eccentricity: | 0.0815213 |
| inclination: | 67.6275° |
| perigee height: | 902 km |
| apogee height: | 2195 km |
| right ascension of ascending node: | 35.1920° |
| argument of perigee: | 47.0407° |
| revolutions per day: | 12.30149922 |
| mean anomaly at epoch: | 348.0216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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