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 61972U 26145.36757610 +.00000000 +00000-0 +37616-3 0 00007
2 61972 43.0007 107.0591 0001368 265.2962 94.7733 15.27585843 05
| Epoch (UTC): | 25 May 2026 08:49:18 |
| Eccentricity: | 0.0001368 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.0591° |
| argument of perigee: | 265.2962° |
| revolutions per day: | 15.27585843 |
| mean anomaly at epoch: | 94.7733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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