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 58922U 26145.64799641 +.00000000 +00000-0 +42225-3 0 00001
2 58922 97.3044 210.8737 0014298 119.0618 241.2052 15.21643548 08
| Epoch (UTC): | 25 May 2026 15:33:06 |
| Eccentricity: | 0.0014298 |
| inclination: | 97.3044° |
| perigee height: | 491 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 210.8737° |
| argument of perigee: | 119.0618° |
| revolutions per day: | 15.21643548 |
| mean anomaly at epoch: | 241.2052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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