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 61244U 26145.13567867 +.00000000 +00000-0 +27808-4 0 00000
2 61244 53.1590 39.3806 0000966 89.7139 270.3990 15.69697708 07
| Epoch (UTC): | 25 May 2026 03:15:22 |
| Eccentricity: | 0.0000966 |
| inclination: | 53.1590° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 39.3806° |
| argument of perigee: | 89.7139° |
| revolutions per day: | 15.69697708 |
| mean anomaly at epoch: | 270.3990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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