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 14241U 26065.53542138 +.00000000 +00000-0 +12747-3 0 00009
2 14241 74.0601 163.2980 0016381 165.7233 194.4387 14.37524159 04
| Epoch (UTC): | 06 March 2026 12:51:00 |
| Eccentricity: | 0.0016381 |
| inclination: | 74.0601° |
| perigee height: | 755 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 163.2980° |
| argument of perigee: | 165.7233° |
| revolutions per day: | 14.37524159 |
| mean anomaly at epoch: | 194.4387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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