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 60321U 26145.45846272 +.00000000 +00000-0 -11766-3 0 00006
2 60321 53.1613 300.4996 0001118 74.3882 285.7242 15.30210821 00
| Epoch (UTC): | 25 May 2026 11:00:11 |
| Eccentricity: | 0.0001118 |
| inclination: | 53.1613° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.4996° |
| argument of perigee: | 74.3882° |
| revolutions per day: | 15.30210821 |
| mean anomaly at epoch: | 285.7242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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