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 52894U 26145.36707731 +.00000000 +00000-0 +61124-4 0 00001
2 52894 98.2255 284.9613 0010628 89.7294 270.5124 14.59527776 04
| Epoch (UTC): | 25 May 2026 08:48:35 |
| Eccentricity: | 0.0010628 |
| inclination: | 98.2255° |
| perigee height: | 687 km |
| apogee height: | 702 km |
| right ascension of ascending node: | 284.9613° |
| argument of perigee: | 89.7294° |
| revolutions per day: | 14.59527776 |
| mean anomaly at epoch: | 270.5124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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