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 49469U 26145.46936994 +.00000000 +00000-0 +44200-3 0 00006
2 49469 42.0047 65.9695 0016832 230.1556 129.7807 15.49355221 04
| Epoch (UTC): | 25 May 2026 11:15:53 |
| Eccentricity: | 0.0016832 |
| inclination: | 42.0047° |
| perigee height: | 407 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 65.9695° |
| argument of perigee: | 230.1556° |
| revolutions per day: | 15.49355221 |
| mean anomaly at epoch: | 129.7807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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