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 57679U 26145.58190218 +.00000000 +00000-0 +22732-4 0 00009
2 57679 53.1596 209.4376 0001170 80.3185 279.7948 15.30189235 03
| Epoch (UTC): | 25 May 2026 13:57:56 |
| Eccentricity: | 0.0001170 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.4376° |
| argument of perigee: | 80.3185° |
| revolutions per day: | 15.30189235 |
| mean anomaly at epoch: | 279.7948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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