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 61777U 26145.57870019 +.00000000 +00000-0 +36388-3 0 00007
2 61777 97.3025 18.0024 0014699 9.7152 350.4378 15.44673509 08
| Epoch (UTC): | 25 May 2026 13:53:19 |
| Eccentricity: | 0.0014699 |
| inclination: | 97.3025° |
| perigee height: | 422 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 18.0024° |
| argument of perigee: | 9.7152° |
| revolutions per day: | 15.44673509 |
| mean anomaly at epoch: | 350.4378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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