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 53009U 26145.27854553 +.00000000 +00000-0 +41248-4 0 00000
2 53009 53.2144 100.2993 0001542 73.8193 286.2969 15.08841915 09
| Epoch (UTC): | 25 May 2026 06:41:06 |
| Eccentricity: | 0.0001542 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.2993° |
| argument of perigee: | 73.8193° |
| revolutions per day: | 15.08841915 |
| mean anomaly at epoch: | 286.2969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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