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 68852U 26145.48979446 +.00000000 +00000-0 +70276-3 0 00006
2 68852 97.2850 160.1565 0000154 352.3527 7.7722 15.49249958 04
| Epoch (UTC): | 25 May 2026 11:45:18 |
| Eccentricity: | 0.0000154 |
| inclination: | 97.2850° |
| perigee height: | 419 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 160.1565° |
| argument of perigee: | 352.3527° |
| revolutions per day: | 15.49249958 |
| mean anomaly at epoch: | 7.7722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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