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 59774U 26145.58384027 +.00000000 +00000-0 +33923-3 0 00003
2 59774 97.6456 274.0884 0007647 257.8831 102.1552 15.28228362 07
| Epoch (UTC): | 25 May 2026 14:00:43 |
| Eccentricity: | 0.0007647 |
| inclination: | 97.6456° |
| perigee height: | 476 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 274.0884° |
| argument of perigee: | 257.8831° |
| revolutions per day: | 15.28228362 |
| mean anomaly at epoch: | 102.1552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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