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 58162U 26145.58775256 +.00000000 +00000-0 -12757-4 0 00005
2 58162 53.1601 222.3643 0000960 101.1998 258.9111 15.30186157 00
| Epoch (UTC): | 25 May 2026 14:06:21 |
| Eccentricity: | 0.0000960 |
| inclination: | 53.1601° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.3643° |
| argument of perigee: | 101.1998° |
| revolutions per day: | 15.30186157 |
| mean anomaly at epoch: | 258.9111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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