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 26075.80738744 +.00000000 +00000-0 +10258-3 0 00001
2 33066 48.4415 267.1665 0007266 316.3843 43.6494 14.73113457 04
| Epoch (UTC): | 16 March 2026 19:22:38 |
| Eccentricity: | 0.0007266 |
| inclination: | 48.4415° |
| perigee height: | 646 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 267.1665° |
| argument of perigee: | 316.3843° |
| revolutions per day: | 14.73113457 |
| mean anomaly at epoch: | 43.6494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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