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 68981U 26145.47864647 +.00000000 +00000-0 +13431-3 0 00004
2 68981 97.7386 43.3346 0003564 205.7477 154.3565 14.91040877 07
| Epoch (UTC): | 25 May 2026 11:29:15 |
| Eccentricity: | 0.0003564 |
| inclination: | 97.7386° |
| perigee height: | 592 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 43.3346° |
| argument of perigee: | 205.7477° |
| revolutions per day: | 14.91040877 |
| mean anomaly at epoch: | 154.3565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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