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 56352U 26145.46072563 +.00000000 +00000-0 +24770-4 0 00009
2 56352 97.4458 145.3743 0001872 92.4643 267.6799 15.05649230 04
| Epoch (UTC): | 25 May 2026 11:03:26 |
| Eccentricity: | 0.0001872 |
| inclination: | 97.4458° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.3743° |
| argument of perigee: | 92.4643° |
| revolutions per day: | 15.05649230 |
| mean anomaly at epoch: | 267.6799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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