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 39133U 26145.05964376 +.00000000 +00000-0 +20346-3 0 00008
2 39133 64.8697 332.9418 0019717 245.9275 113.9793 15.25999389 03
| Epoch (UTC): | 25 May 2026 01:25:53 |
| Eccentricity: | 0.0019717 |
| inclination: | 64.8697° |
| perigee height: | 474 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 332.9418° |
| argument of perigee: | 245.9275° |
| revolutions per day: | 15.25999389 |
| mean anomaly at epoch: | 113.9793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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