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 42758U 26145.63650288 +.00000000 +00000-0 +23989-3 0 00009
2 42758 43.0145 308.5912 0031560 359.6803 0.4021 15.18241137 02
| Epoch (UTC): | 25 May 2026 15:16:33 |
| Eccentricity: | 0.0031560 |
| inclination: | 43.0145° |
| perigee height: | 489 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 308.5912° |
| argument of perigee: | 359.6803° |
| revolutions per day: | 15.18241137 |
| mean anomaly at epoch: | 0.4021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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