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 62691U 26145.51015150 +.00000000 +00000-0 +79089-3 0 00009
2 62691 97.3769 230.3192 0000905 262.0552 98.0594 15.44110170 02
| Epoch (UTC): | 25 May 2026 12:14:37 |
| Eccentricity: | 0.0000905 |
| inclination: | 97.3769° |
| perigee height: | 433 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 230.3192° |
| argument of perigee: | 262.0552° |
| revolutions per day: | 15.44110170 |
| mean anomaly at epoch: | 98.0594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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