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 57880U 26145.54280338 +.00000000 +00000-0 +16613-3 0 00002
2 57880 43.0010 210.9566 0001482 269.0312 91.0370 15.27576177 03
| Epoch (UTC): | 25 May 2026 13:01:38 |
| Eccentricity: | 0.0001482 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 210.9566° |
| argument of perigee: | 269.0312° |
| revolutions per day: | 15.27576177 |
| mean anomaly at epoch: | 91.0370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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