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 59521U 26145.33498449 +.00000000 +00000-0 +43079-4 0 00004
2 59521 43.0039 245.5015 0001867 284.5050 75.5595 15.27570909 02
| Epoch (UTC): | 25 May 2026 08:02:22 |
| Eccentricity: | 0.0001867 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 245.5015° |
| argument of perigee: | 284.5050° |
| revolutions per day: | 15.27570909 |
| mean anomaly at epoch: | 75.5595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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