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 53548U 26145.51591066 +.00000000 +00000-0 -45284-5 0 00008
2 53548 53.2123 79.2327 0001216 96.9171 263.1959 15.08835149 05
| Epoch (UTC): | 25 May 2026 12:22:54 |
| Eccentricity: | 0.0001216 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 79.2327° |
| argument of perigee: | 96.9171° |
| revolutions per day: | 15.08835149 |
| mean anomaly at epoch: | 263.1959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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