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 61068U 26145.27838145 +.00000000 +00000-0 +40377-4 0 00005
2 61068 53.1620 95.3736 0001302 82.6402 277.4747 15.31704839 00
| Epoch (UTC): | 25 May 2026 06:40:52 |
| Eccentricity: | 0.0001302 |
| inclination: | 53.1620° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.3736° |
| argument of perigee: | 82.6402° |
| revolutions per day: | 15.31704839 |
| mean anomaly at epoch: | 277.4747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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