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 46698U 26145.39331162 +.00000000 +00000-0 +60020-3 0 00003
2 46698 53.0405 194.5863 0007193 357.1374 2.9599 15.66462717 07
| Epoch (UTC): | 25 May 2026 09:26:22 |
| Eccentricity: | 0.0007193 |
| inclination: | 53.0405° |
| perigee height: | 364 km |
| apogee height: | 374 km |
| right ascension of ascending node: | 194.5863° |
| argument of perigee: | 357.1374° |
| revolutions per day: | 15.66462717 |
| mean anomaly at epoch: | 2.9599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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