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 61907U 26145.65010691 +.00000000 +00000-0 +19318-3 0 00007
2 61907 97.4133 218.5944 0013325 132.4541 227.7821 15.16952346 00
| Epoch (UTC): | 25 May 2026 15:36:09 |
| Eccentricity: | 0.0013325 |
| inclination: | 97.4133° |
| perigee height: | 506 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 218.5944° |
| argument of perigee: | 132.4541° |
| revolutions per day: | 15.16952346 |
| mean anomaly at epoch: | 227.7821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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