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 53708U 26145.57616722 +.00000000 +00000-0 -33120-4 0 00004
2 53708 53.2127 243.8287 0001481 83.2213 276.8948 15.08828679 00
| Epoch (UTC): | 25 May 2026 13:49:40 |
| Eccentricity: | 0.0001481 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 243.8287° |
| argument of perigee: | 83.2213° |
| revolutions per day: | 15.08828679 |
| mean anomaly at epoch: | 276.8948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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