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 54015U 26145.45887956 +.00000000 +00000-0 +75702-4 0 00003
2 54015 53.2165 219.4042 0001322 79.0665 281.0475 15.08836150 06
| Epoch (UTC): | 25 May 2026 11:00:47 |
| Eccentricity: | 0.0001322 |
| inclination: | 53.2165° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 219.4042° |
| argument of perigee: | 79.0665° |
| revolutions per day: | 15.08836150 |
| mean anomaly at epoch: | 281.0475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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