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 61242U 26145.60160862 +.00000000 +00000-0 +21473-3 0 00005
2 61242 97.4462 156.6099 0011781 320.4004 39.6373 15.27242963 08
| Epoch (UTC): | 25 May 2026 14:26:18 |
| Eccentricity: | 0.0011781 |
| inclination: | 97.4462° |
| perigee height: | 476 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 156.6099° |
| argument of perigee: | 320.4004° |
| revolutions per day: | 15.27242963 |
| mean anomaly at epoch: | 39.6373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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