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 33066U 26074.58646267 +.00000000 +00000-0 +10231-3 0 00004
2 33066 48.4415 272.9100 0007307 311.4822 48.5463 14.73111555 08
| Epoch (UTC): | 15 March 2026 14:04:30 |
| Eccentricity: | 0.0007307 |
| inclination: | 48.4415° |
| perigee height: | 646 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 272.9100° |
| argument of perigee: | 311.4822° |
| revolutions per day: | 14.73111555 |
| mean anomaly at epoch: | 48.5463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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