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 68732U 26145.58335647 +.00000000 +00000-0 +14618-2 0 00000
2 68732 97.2850 9.1463 0001527 95.6242 29.8790 15.49146228 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001527 |
| inclination: | 97.2850° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 9.1463° |
| argument of perigee: | 95.6242° |
| revolutions per day: | 15.49146228 |
| mean anomaly at epoch: | 29.8790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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