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 68949U 26145.37631383 +.00000000 +00000-0 -13891-3 0 00007
2 68949 51.8735 178.3534 0019526 71.3525 288.9577 15.29742126 09
| Epoch (UTC): | 25 May 2026 09:01:53 |
| Eccentricity: | 0.0019526 |
| inclination: | 51.8735° |
| perigee height: | 463 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 178.3534° |
| argument of perigee: | 71.3525° |
| revolutions per day: | 15.29742126 |
| mean anomaly at epoch: | 288.9577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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