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 33409U 26042.29479785 +.00000000 +00000-0 +19283-3 0 00003
2 33409 97.8686 60.0872 0021698 104.1643 256.1994 15.03678650 00
| Epoch (UTC): | 11 February 2026 07:04:30 |
| Eccentricity: | 0.0021698 |
| inclination: | 97.8686° |
| perigee height: | 541 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 60.0872° |
| argument of perigee: | 104.1643° |
| revolutions per day: | 15.03678650 |
| mean anomaly at epoch: | 256.1994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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