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 53640U 26145.56010985 +.00000000 +00000-0 -65534-3 0 00000
2 53640 53.2120 238.7840 0001621 71.2053 288.9115 15.08753897 00
| Epoch (UTC): | 25 May 2026 13:26:33 |
| Eccentricity: | 0.0001621 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 238.7840° |
| argument of perigee: | 71.2053° |
| revolutions per day: | 15.08753897 |
| mean anomaly at epoch: | 288.9115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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