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 68247U 26145.15435876 +.00000000 +00000-0 +98596-3 0 00007
2 68247 53.1586 297.8260 0000889 114.1122 245.9980 15.49357185 03
| Epoch (UTC): | 25 May 2026 03:42:16 |
| Eccentricity: | 0.0000889 |
| inclination: | 53.1586° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 297.8260° |
| argument of perigee: | 114.1122° |
| revolutions per day: | 15.49357185 |
| mean anomaly at epoch: | 245.9980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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