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 45712U 26145.37961881 +.00000000 +00000-0 +89839-3 0 00003
2 45712 53.0527 22.9395 0003398 67.8992 292.2369 15.33063018 00
| Epoch (UTC): | 25 May 2026 09:06:39 |
| Eccentricity: | 0.0003398 |
| inclination: | 53.0527° |
| perigee height: | 464 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 22.9395° |
| argument of perigee: | 67.8992° |
| revolutions per day: | 15.33063018 |
| mean anomaly at epoch: | 292.2369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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