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 53501U 26145.66668980 +.00000000 +00000-0 +90734-2 0 00009
2 53501 97.6047 267.7624 0000968 82.1594 36.7719 15.39242436 07
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000968 |
| inclination: | 97.6047° |
| perigee height: | 448 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 267.7624° |
| argument of perigee: | 82.1594° |
| revolutions per day: | 15.39242436 |
| mean anomaly at epoch: | 36.7719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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