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 68078U 26145.48589470 +.00000000 +00000-0 +52930-3 0 00007
2 68078 53.1593 181.2554 0001314 46.0911 314.0200 15.34403385 09
| Epoch (UTC): | 25 May 2026 11:39:41 |
| Eccentricity: | 0.0001314 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 181.2554° |
| argument of perigee: | 46.0911° |
| revolutions per day: | 15.34403385 |
| mean anomaly at epoch: | 314.0200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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