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 58652U 26140.76547388 +.00000000 +00000-0 +80671-4 0 00006
2 58652 97.4033 109.9068 0001696 106.4949 253.6461 14.98098494 05
| Epoch (UTC): | 20 May 2026 18:22:16 |
| Eccentricity: | 0.0001696 |
| inclination: | 97.4033° |
| perigee height: | 572 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 109.9068° |
| argument of perigee: | 106.4949° |
| revolutions per day: | 14.98098494 |
| mean anomaly at epoch: | 253.6461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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