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 26145.61650110 +.00000000 +00000-0 +61245-4 0 00002
2 33409 97.8573 165.1352 0020610 115.0663 245.2705 15.04222272 06
| Epoch (UTC): | 25 May 2026 14:47:45 |
| Eccentricity: | 0.0020610 |
| inclination: | 97.8573° |
| perigee height: | 540 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 165.1352° |
| argument of perigee: | 115.0663° |
| revolutions per day: | 15.04222272 |
| mean anomaly at epoch: | 245.2705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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