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 55449U 26145.35666156 +.00000000 +00000-0 +24266-4 0 00000
2 55449 43.0003 256.0656 0000836 297.5049 62.5717 15.27579548 03
| Epoch (UTC): | 25 May 2026 08:33:35 |
| Eccentricity: | 0.0000836 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 256.0656° |
| argument of perigee: | 297.5049° |
| revolutions per day: | 15.27579548 |
| mean anomaly at epoch: | 62.5717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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