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 68258U 26145.43839712 +.00000000 +00000-0 +96084-3 0 00007
2 68258 53.1587 300.3144 0001087 90.5076 269.6050 15.30223102 05
| Epoch (UTC): | 25 May 2026 10:31:17 |
| Eccentricity: | 0.0001087 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.3144° |
| argument of perigee: | 90.5076° |
| revolutions per day: | 15.30223102 |
| mean anomaly at epoch: | 269.6050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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