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 53176U 26145.46575815 +.00000000 +00000-0 +75162-4 0 00009
2 53176 53.2115 164.3717 0000964 67.4451 292.6643 15.08832666 03
| Epoch (UTC): | 25 May 2026 11:10:41 |
| Eccentricity: | 0.0000964 |
| inclination: | 53.2115° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 164.3717° |
| argument of perigee: | 67.4451° |
| revolutions per day: | 15.08832666 |
| mean anomaly at epoch: | 292.6643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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