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 68262U 26145.58335647 +.00000000 +00000-0 +27966-4 0 00000
2 68262 53.1595 321.1944 0001003 82.6638 20.6008 15.34394124 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001003 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 321.1944° |
| argument of perigee: | 82.6638° |
| revolutions per day: | 15.34394124 |
| mean anomaly at epoch: | 20.6008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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