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 68929U 26145.50942017 +.00000000 +00000-0 -13492-2 0 00005
2 68929 51.8745 177.7486 0022444 67.8300 292.5062 15.29422764 04
| Epoch (UTC): | 25 May 2026 12:13:33 |
| Eccentricity: | 0.0022444 |
| inclination: | 51.8745° |
| perigee height: | 462 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 177.7486° |
| argument of perigee: | 67.8300° |
| revolutions per day: | 15.29422764 |
| mean anomaly at epoch: | 292.5062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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