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 60372U 26145.50115766 +.00000000 +00000-0 +99061-5 0 00000
2 60372 53.1607 313.1182 0001191 99.2274 260.8862 15.30202064 01
| Epoch (UTC): | 25 May 2026 12:01:40 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.1182° |
| argument of perigee: | 99.2274° |
| revolutions per day: | 15.30202064 |
| mean anomaly at epoch: | 260.8862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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