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 53215U 26145.45238638 +.00000000 +00000-0 -93176-4 0 00007
2 53215 97.4491 206.5168 0001721 124.5984 235.5406 15.05656161 05
| Epoch (UTC): | 25 May 2026 10:51:26 |
| Eccentricity: | 0.0001721 |
| inclination: | 97.4491° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.5168° |
| argument of perigee: | 124.5984° |
| revolutions per day: | 15.05656161 |
| mean anomaly at epoch: | 235.5406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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