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 62076U 26145.37431242 +.00000000 +00000-0 +53445-3 0 00002
2 62076 53.1598 184.8095 0001633 93.2971 266.8216 15.30211757 06
| Epoch (UTC): | 25 May 2026 08:59:00 |
| Eccentricity: | 0.0001633 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.8095° |
| argument of perigee: | 93.2971° |
| revolutions per day: | 15.30211757 |
| mean anomaly at epoch: | 266.8216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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