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 53864U 26145.43305513 +.00000000 +00000-0 +14104-4 0 00005
2 53864 53.2139 299.1715 0001320 83.4067 276.7075 15.08838800 04
| Epoch (UTC): | 25 May 2026 10:23:35 |
| Eccentricity: | 0.0001320 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 299.1715° |
| argument of perigee: | 83.4067° |
| revolutions per day: | 15.08838800 |
| mean anomaly at epoch: | 276.7075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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