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 68195U 26145.35887646 +.00000000 +00000-0 +89004-3 0 00001
2 68195 53.1570 269.7641 0001112 79.8942 280.2186 15.34415864 09
| Epoch (UTC): | 25 May 2026 08:36:46 |
| Eccentricity: | 0.0001112 |
| inclination: | 53.1570° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 269.7641° |
| argument of perigee: | 79.8942° |
| revolutions per day: | 15.34415864 |
| mean anomaly at epoch: | 280.2186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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