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 37179U 26145.61158550 +.00000000 +00000-0 +32454-3 0 00000
2 37179 97.8297 168.0302 0017112 306.7328 53.2333 15.17672169 06
| Epoch (UTC): | 25 May 2026 14:40:40 |
| Eccentricity: | 0.0017112 |
| inclination: | 97.8297° |
| perigee height: | 501 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 168.0302° |
| argument of perigee: | 306.7328° |
| revolutions per day: | 15.17672169 |
| mean anomaly at epoch: | 53.2333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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