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 26150.53901625 +.00000000 +00000-0 +22845-3 0 00001
2 33409 97.8568 170.1376 0020554 99.9672 260.3874 15.04248685 00
| Epoch (UTC): | 30 May 2026 12:56:11 |
| Eccentricity: | 0.0020554 |
| inclination: | 97.8568° |
| perigee height: | 540 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 170.1376° |
| argument of perigee: | 99.9672° |
| revolutions per day: | 15.04248685 |
| mean anomaly at epoch: | 260.3874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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