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 57819U 26145.45179178 +.00000000 +00000-0 +48443-4 0 00000
2 57819 43.0022 161.0489 0001500 266.6224 93.4456 15.27579771 08
| Epoch (UTC): | 25 May 2026 10:50:34 |
| Eccentricity: | 0.0001500 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 161.0489° |
| argument of perigee: | 266.6224° |
| revolutions per day: | 15.27579771 |
| mean anomaly at epoch: | 93.4456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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