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 68828U 26145.37002688 +.00000000 +00000-0 +16747-3 0 00005
2 68828 96.6463 63.8756 0018092 121.8658 238.4376 15.81598794 04
| Epoch (UTC): | 25 May 2026 08:52:50 |
| Eccentricity: | 0.0018092 |
| inclination: | 96.6463° |
| perigee height: | 314 km |
| apogee height: | 338 km |
| right ascension of ascending node: | 63.8756° |
| argument of perigee: | 121.8658° |
| revolutions per day: | 15.81598794 |
| mean anomaly at epoch: | 238.4376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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