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 60021U 26145.52354778 +.00000000 +00000-0 -19755-5 0 00004
2 60021 53.1613 77.5663 0001170 97.0109 263.1027 15.34390998 01
| Epoch (UTC): | 25 May 2026 12:33:54 |
| Eccentricity: | 0.0001170 |
| inclination: | 53.1613° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 77.5663° |
| argument of perigee: | 97.0109° |
| revolutions per day: | 15.34390998 |
| mean anomaly at epoch: | 263.1027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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