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 68937U 26145.46591632 +.00000000 +00000-0 -77553-3 0 00001
2 68937 51.8756 177.4698 0012366 64.8991 295.3276 15.32560381 02
| Epoch (UTC): | 25 May 2026 11:10:55 |
| Eccentricity: | 0.0012366 |
| inclination: | 51.8756° |
| perigee height: | 460 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 177.4698° |
| argument of perigee: | 64.8991° |
| revolutions per day: | 15.32560381 |
| mean anomaly at epoch: | 295.3276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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