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 00011U 26073.66954295 +.00000000 +00000-0 +51051-3 0 00004
2 00011 32.8745 82.8189 1445786 239.0264 106.0394 11.90278180 00
| Epoch (UTC): | 14 March 2026 16:04:08 |
| Eccentricity: | 0.1445786 |
| inclination: | 32.8745° |
| perigee height: | 553 km |
| apogee height: | 2896 km |
| right ascension of ascending node: | 82.8189° |
| argument of perigee: | 239.0264° |
| revolutions per day: | 11.90278180 |
| mean anomaly at epoch: | 106.0394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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