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 57760U 26088.19055172 +.00000000 +00000-0 +20782-3 0 00004
2 57760 80.9952 75.0524 0163548 183.4641 176.5427 14.34787223 00
| Epoch (UTC): | 29 March 2026 04:34:23 |
| Eccentricity: | 0.0163548 |
| inclination: | 80.9952° |
| perigee height: | 659 km |
| apogee height: | 893 km |
| right ascension of ascending node: | 75.0524° |
| argument of perigee: | 183.4641° |
| revolutions per day: | 14.34787223 |
| mean anomaly at epoch: | 176.5427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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