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 53898U 26145.56187615 +.00000000 +00000-0 -52315-4 0 00004
2 53898 53.2122 338.7463 0001689 94.7240 265.3945 15.08839877 04
| Epoch (UTC): | 25 May 2026 13:29:06 |
| Eccentricity: | 0.0001689 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 338.7463° |
| argument of perigee: | 94.7240° |
| revolutions per day: | 15.08839877 |
| mean anomaly at epoch: | 265.3945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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