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 68512U 26145.33846251 +.00000000 +00000-0 +11796-2 0 00001
2 68512 53.1575 127.2087 0001148 111.2258 248.8874 15.49323815 03
| Epoch (UTC): | 25 May 2026 08:07:23 |
| Eccentricity: | 0.0001148 |
| inclination: | 53.1575° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 127.2087° |
| argument of perigee: | 111.2258° |
| revolutions per day: | 15.49323815 |
| mean anomaly at epoch: | 248.8874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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