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 49143U 26145.22472199 +.00000000 +00000-0 +76615-4 0 00007
2 49143 70.0002 82.5186 0003150 263.8820 96.1979 14.97534983 04
| Epoch (UTC): | 25 May 2026 05:23:35 |
| Eccentricity: | 0.0003150 |
| inclination: | 70.0002° |
| perigee height: | 572 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 82.5186° |
| argument of perigee: | 263.8820° |
| revolutions per day: | 14.97534983 |
| mean anomaly at epoch: | 96.1979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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