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 59896U 26145.44023178 +.00000000 +00000-0 +79205-4 0 00004
2 59896 43.0048 48.5996 0001690 275.9151 84.1508 15.27581161 08
| Epoch (UTC): | 25 May 2026 10:33:56 |
| Eccentricity: | 0.0001690 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.5996° |
| argument of perigee: | 275.9151° |
| revolutions per day: | 15.27581161 |
| mean anomaly at epoch: | 84.1508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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