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 68561U 26145.00002315 +.00000000 +00000-0 +12978-2 0 00007
2 68561 53.1589 7.4686 0000181 6.3032 131.7076 15.34365104 01
| Epoch (UTC): | 25 May 2026 00:00:02 |
| Eccentricity: | 0.0000181 |
| inclination: | 53.1589° |
| perigee height: | 463 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 7.4686° |
| argument of perigee: | 6.3032° |
| revolutions per day: | 15.34365104 |
| mean anomaly at epoch: | 131.7076° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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