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 62588U 26145.03229662 +.00000000 +00000-0 +13759-2 0 00007
2 62588 43.0038 25.7567 0002345 266.3833 93.6767 15.70873072 04
| Epoch (UTC): | 25 May 2026 00:46:30 |
| Eccentricity: | 0.0002345 |
| inclination: | 43.0038° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 25.7567° |
| argument of perigee: | 266.3833° |
| revolutions per day: | 15.70873072 |
| mean anomaly at epoch: | 93.6767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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