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 57889U 26145.65537904 +.00000000 +00000-0 +30727-3 0 00009
2 57889 34.9919 4.7719 0003925 225.5625 134.4767 15.17581103 02
| Epoch (UTC): | 25 May 2026 15:43:44 |
| Eccentricity: | 0.0003925 |
| inclination: | 34.9919° |
| perigee height: | 510 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 4.7719° |
| argument of perigee: | 225.5625° |
| revolutions per day: | 15.17581103 |
| mean anomaly at epoch: | 134.4767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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