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 57187U 26088.18780132 +.00000000 +00000-0 +58375-3 0 00006
2 57187 97.5173 151.6155 0009852 23.6197 336.5491 15.25218997 08
| Epoch (UTC): | 29 March 2026 04:30:26 |
| Eccentricity: | 0.0009852 |
| inclination: | 97.5173° |
| perigee height: | 483 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 151.6155° |
| argument of perigee: | 23.6197° |
| revolutions per day: | 15.25218997 |
| mean anomaly at epoch: | 336.5491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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