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 61240U 26145.60449817 +.00000000 +00000-0 +16744-3 0 00008
2 61240 97.4423 153.8891 0000508 29.8121 330.3142 15.18700167 07
| Epoch (UTC): | 25 May 2026 14:30:28 |
| Eccentricity: | 0.0000508 |
| inclination: | 97.4423° |
| perigee height: | 509 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 153.8891° |
| argument of perigee: | 29.8121° |
| revolutions per day: | 15.18700167 |
| mean anomaly at epoch: | 330.3142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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