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 60129U 26144.95720579 +.00000000 +00000-0 +52738-4 0 00001
2 60129 53.1611 30.3026 0001222 81.9151 278.1988 15.30196703 01
| Epoch (UTC): | 24 May 2026 22:58:22 |
| Eccentricity: | 0.0001222 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.3026° |
| argument of perigee: | 81.9151° |
| revolutions per day: | 15.30196703 |
| mean anomaly at epoch: | 278.1988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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