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 53177U 26145.29740444 +.00000000 +00000-0 +72310-4 0 00005
2 53177 53.2150 155.2003 0001140 80.1747 279.9374 15.08841292 01
| Epoch (UTC): | 25 May 2026 07:08:15 |
| Eccentricity: | 0.0001140 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 155.2003° |
| argument of perigee: | 80.1747° |
| revolutions per day: | 15.08841292 |
| mean anomaly at epoch: | 279.9374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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