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 53798U 26145.40822029 +.00000000 +00000-0 -28342-4 0 00004
2 53798 53.2126 289.3180 0001669 102.6723 257.4456 15.08839758 04
| Epoch (UTC): | 25 May 2026 09:47:50 |
| Eccentricity: | 0.0001669 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 289.3180° |
| argument of perigee: | 102.6723° |
| revolutions per day: | 15.08839758 |
| mean anomaly at epoch: | 257.4456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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