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 68939U 26145.46484829 +.00000000 +00000-0 +56760-3 0 00008
2 68939 51.8742 177.4615 0011236 66.6161 293.6004 15.32836592 02
| Epoch (UTC): | 25 May 2026 11:09:22 |
| Eccentricity: | 0.0011236 |
| inclination: | 51.8742° |
| perigee height: | 460 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 177.4615° |
| argument of perigee: | 66.6161° |
| revolutions per day: | 15.32836592 |
| mean anomaly at epoch: | 293.6004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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