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 57872U 26145.45625947 +.00000000 +00000-0 +52296-4 0 00000
2 57872 43.0043 197.5385 0001426 265.5964 94.4725 15.27577182 09
| Epoch (UTC): | 25 May 2026 10:57:00 |
| Eccentricity: | 0.0001426 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.5385° |
| argument of perigee: | 265.5964° |
| revolutions per day: | 15.27577182 |
| mean anomaly at epoch: | 94.4725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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