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 53209U 26145.12427650 +.00000000 +00000-0 -58699-3 0 00008
2 53209 97.4487 205.1492 0000291 85.2031 274.9230 15.05702557 08
| Epoch (UTC): | 25 May 2026 02:58:57 |
| Eccentricity: | 0.0000291 |
| inclination: | 97.4487° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 205.1492° |
| argument of perigee: | 85.2031° |
| revolutions per day: | 15.05702557 |
| mean anomaly at epoch: | 274.9230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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